1 00:00:00,030 --> 00:00:02,470 The following content is provided under a Creative 2 00:00:02,470 --> 00:00:04,000 Commons license. 3 00:00:04,000 --> 00:00:06,330 Your support will help MIT OpenCourseWare 4 00:00:06,330 --> 00:00:10,680 continue to offer high quality educational resources for free. 5 00:00:10,680 --> 00:00:13,300 To make a donation, or view additional materials 6 00:00:13,300 --> 00:00:17,025 from hundreds of MIT courses, visit MIT OpenCourseWare 7 00:00:17,025 --> 00:00:17,650 at ocw.mit.edu. 8 00:00:26,540 --> 00:00:29,100 LORNA GIBSON: All right, so last time we 9 00:00:29,100 --> 00:00:31,560 started talking about energy absorption, 10 00:00:31,560 --> 00:00:33,920 and I wanted to try to finish that up today. 11 00:00:33,920 --> 00:00:36,460 And then next week we would talk about sandwich panels 12 00:00:36,460 --> 00:00:39,990 and using honeycombs and foams in sandwich panels. 13 00:00:39,990 --> 00:00:42,140 So I think we got as far as the idea 14 00:00:42,140 --> 00:00:45,470 of introducing what these energy absorption diagrams are. 15 00:00:45,470 --> 00:00:48,180 So let me run through this little sequence again, 16 00:00:48,180 --> 00:00:50,480 and then I'll put the notes up on the board. 17 00:00:50,480 --> 00:00:54,350 So the idea is that you have your compressive stress strain 18 00:00:54,350 --> 00:00:57,140 curve-- so here's a series of curves for different densities 19 00:00:57,140 --> 00:00:58,230 of a foam. 20 00:00:58,230 --> 00:01:00,500 And we would do these all at the same strain 21 00:01:00,500 --> 00:01:03,170 rate and temperature, so that those aren't variables. 22 00:01:03,170 --> 00:01:06,370 And then what we would do is we could turn those into energy 23 00:01:06,370 --> 00:01:07,720 absorption diagrams. 24 00:01:07,720 --> 00:01:10,200 So notice here, this is a log plot. 25 00:01:10,200 --> 00:01:12,250 So here's that energy absorption here. 26 00:01:12,250 --> 00:01:14,650 Here's the peak stress here-- so that's 27 00:01:14,650 --> 00:01:18,620 the peak stress up to some level of energy that you've absorbed. 28 00:01:18,620 --> 00:01:22,470 And we've normalized both of those by the solid modulus. 29 00:01:22,470 --> 00:01:25,160 So say we look at one density here, say we look at the lowest 30 00:01:25,160 --> 00:01:26,540 density-- 0.01. 31 00:01:26,540 --> 00:01:30,410 So here's our curve here for the test. 32 00:01:30,410 --> 00:01:33,000 If I go up to some stress level that's 33 00:01:33,000 --> 00:01:35,120 still in the linear elastic region, 34 00:01:35,120 --> 00:01:38,570 then that's going to translate into somewhere along here 35 00:01:38,570 --> 00:01:40,165 on the energy absorption curve. 36 00:01:40,165 --> 00:01:41,540 And one of the things we're going 37 00:01:41,540 --> 00:01:43,850 to do today-- I'm going to show you how you draw these, 38 00:01:43,850 --> 00:01:46,410 and how you can set them up. 39 00:01:46,410 --> 00:01:48,810 And you can either get them from experiments-- 40 00:01:48,810 --> 00:01:52,290 so this is, say the top curve were experiments, doing it 41 00:01:52,290 --> 00:01:57,020 from experiments-- or you can use the models for the foams 42 00:01:57,020 --> 00:01:57,930 to do it, as well. 43 00:01:57,930 --> 00:02:00,150 So we'll see how you can do from both ways. 44 00:02:00,150 --> 00:02:02,150 So this would be the linear elastic bit here. 45 00:02:02,150 --> 00:02:04,720 This vertical part-- where the energy is increasing, 46 00:02:04,720 --> 00:02:07,050 but the peak stress isn't increasing-- that corresponds 47 00:02:07,050 --> 00:02:08,940 to the plateau here. 48 00:02:08,940 --> 00:02:11,700 And then this part here, where the energy is not 49 00:02:11,700 --> 00:02:13,670 increasing very much, but the stress increases 50 00:02:13,670 --> 00:02:18,010 a lot-- that corresponds to the densification part over there. 51 00:02:18,010 --> 00:02:20,330 So what you would do is you would do tests 52 00:02:20,330 --> 00:02:23,340 on foams of different densities, and from the test data, 53 00:02:23,340 --> 00:02:25,170 you could draw an energy absorption 54 00:02:25,170 --> 00:02:27,150 curve for each density. 55 00:02:27,150 --> 00:02:29,590 So you plot-- there's four different densities here, 56 00:02:29,590 --> 00:02:32,446 so it forms a family of these curves. 57 00:02:32,446 --> 00:02:33,820 And then what you do is you say-- 58 00:02:33,820 --> 00:02:35,810 and I think we talked with this last time-- 59 00:02:35,810 --> 00:02:38,630 that the place you want to be is at this shoulder point. 60 00:02:38,630 --> 00:02:41,770 You want to be absorbing as much energy as possible 61 00:02:41,770 --> 00:02:43,344 at that plateau stress. 62 00:02:43,344 --> 00:02:45,760 So you want to be at the point just before it turns around 63 00:02:45,760 --> 00:02:47,730 to the densification regime. 64 00:02:47,730 --> 00:02:50,330 So you can mark that little shoulder point 65 00:02:50,330 --> 00:02:51,130 for each density. 66 00:02:51,130 --> 00:02:54,390 So here's like 0.01, here's 0.03, and so on. 67 00:02:54,390 --> 00:02:57,320 And then those points can be connected by a line-- 68 00:02:57,320 --> 00:03:00,470 so that heavy line then connects those shoulder points, 69 00:03:00,470 --> 00:03:02,350 or those optimum points. 70 00:03:02,350 --> 00:03:06,010 And then what you can do is then repeat this whole process 71 00:03:06,010 --> 00:03:07,670 for different strain rates. 72 00:03:07,670 --> 00:03:11,260 So this family of lines here is at different strain rates-- 73 00:03:11,260 --> 00:03:15,166 so this set that goes this way, corresponds to this line here. 74 00:03:15,166 --> 00:03:17,040 And if you do them at different strain rates, 75 00:03:17,040 --> 00:03:20,730 where the shoulder appears at a slightly different point-- 76 00:03:20,730 --> 00:03:22,900 and so if you mark those shorter points, 77 00:03:22,900 --> 00:03:25,690 you can draw these lines here that connect up 78 00:03:25,690 --> 00:03:27,680 for one relative density. 79 00:03:27,680 --> 00:03:30,820 So this line on the left hand side here, 80 00:03:30,820 --> 00:03:33,450 these are all relative densities of 0.01, 81 00:03:33,450 --> 00:03:36,020 these ones are all relative densities of 0.03. 82 00:03:36,020 --> 00:03:38,800 So this diagram down here, doesn't really 83 00:03:38,800 --> 00:03:40,360 look like this at all-- it doesn't 84 00:03:40,360 --> 00:03:42,990 look like the basic energy absorption diagram. 85 00:03:42,990 --> 00:03:44,950 But it actually has information for what 86 00:03:44,950 --> 00:03:47,620 the optimum would be for a range of densities 87 00:03:47,620 --> 00:03:49,700 and a range of strain rates. 88 00:03:49,700 --> 00:03:52,500 So typically, these foams are viscoelastic 89 00:03:52,500 --> 00:03:54,300 and they have some strain rate sensitivity. 90 00:03:54,300 --> 00:03:57,200 So you'd like to get the strain rate sensitivity into it. 91 00:03:57,200 --> 00:03:58,870 And it's not shown here, but you could 92 00:03:58,870 --> 00:04:00,840 do the same thing at a constant strain rate 93 00:04:00,840 --> 00:04:02,240 and varying the temperature, too. 94 00:04:02,240 --> 00:04:04,198 So if you had things at different temperatures, 95 00:04:04,198 --> 00:04:05,910 you could do the same kind of idea. 96 00:04:05,910 --> 00:04:08,730 OK-- so are we good with how this works? 97 00:04:08,730 --> 00:04:11,140 Because now I'm going to write some notes on the board 98 00:04:11,140 --> 00:04:13,335 so you have it in your notes. 99 00:04:37,560 --> 00:04:41,300 So the idea is that you turn your stress strain curve 100 00:04:41,300 --> 00:04:44,860 to look something like that, into an energy absorption 101 00:04:44,860 --> 00:04:46,070 diagram. 102 00:04:46,070 --> 00:04:56,130 And you can plot on log log scales, the energy 103 00:04:56,130 --> 00:04:57,520 versus the peak stress. 104 00:04:57,520 --> 00:04:59,380 And you get something like that. 105 00:04:59,380 --> 00:05:02,666 And this point here, I'm going to call the shoulder point. 106 00:05:07,970 --> 00:05:10,920 And that would use the material in the most efficient way-- 107 00:05:10,920 --> 00:05:13,530 you get the most energy absorption without getting 108 00:05:13,530 --> 00:05:15,147 higher than that plateau stress. 109 00:05:18,490 --> 00:05:24,390 So we can say at this stress plateau, the energy increases 110 00:05:24,390 --> 00:05:26,345 without much increase in the peak stress. 111 00:05:44,670 --> 00:05:50,680 And then as the foam densifies, then you 112 00:05:50,680 --> 00:05:56,010 get an increase in that peak stress, 113 00:05:56,010 --> 00:05:58,190 with little increase in the energy absorbed. 114 00:06:07,890 --> 00:06:10,210 And so ideally, you want to be at that shoulder point. 115 00:06:25,350 --> 00:06:28,160 So to construct these energy diagrams, 116 00:06:28,160 --> 00:06:32,220 you can test the series of foams at different relative densities 117 00:06:32,220 --> 00:06:35,320 and constant strain rate and temperature. 118 00:06:56,140 --> 00:06:59,950 And then you make that plot of the energy absorbed 119 00:06:59,950 --> 00:07:06,170 normalized by the solid modulus, versus the peak stress 120 00:07:06,170 --> 00:07:09,020 normalized by the solid modulus for each curve. 121 00:07:14,880 --> 00:07:17,720 And typically what people do is they would take 122 00:07:17,720 --> 00:07:22,776 the solid modulus at a constant strain rate and temperature, 123 00:07:22,776 --> 00:07:24,651 so you don't have to introduce that, as well. 124 00:07:34,054 --> 00:07:36,470 Then you would mark the density for each of those shoulder 125 00:07:36,470 --> 00:07:41,010 points, and then you would connect them. 126 00:07:53,070 --> 00:07:55,000 And then you could repeat this whole process 127 00:07:55,000 --> 00:07:56,320 for different strain rates. 128 00:08:06,360 --> 00:08:08,870 And then you would draw the final diagram 129 00:08:08,870 --> 00:08:11,390 at the bottom, where you have this family of lines that 130 00:08:11,390 --> 00:08:14,486 describes the shoulder points for different densities 131 00:08:14,486 --> 00:08:15,610 and different strain rates. 132 00:08:45,542 --> 00:08:48,000 And you could treat different temperatures in the same way, 133 00:08:48,000 --> 00:08:48,790 if you wanted to. 134 00:08:48,790 --> 00:08:50,456 You would hold the strain rate constant, 135 00:08:50,456 --> 00:08:53,240 and vary the temperature. 136 00:08:53,240 --> 00:08:54,990 so it's kind of a nice way of just putting 137 00:08:54,990 --> 00:08:56,490 a lot of information in one diagram. 138 00:08:58,780 --> 00:09:00,900 So one of the things about this is 139 00:09:00,900 --> 00:09:04,240 that, because we're normalizing by Es, 140 00:09:04,240 --> 00:09:08,210 and if you think of elastomeric foams, elastomeric foams, 141 00:09:08,210 --> 00:09:10,960 both the Young's modulus depends on Es, 142 00:09:10,960 --> 00:09:13,500 and the plateau stress depends Es. 143 00:09:13,500 --> 00:09:16,290 So the Young's modulus depends on the stiffness of the solid, 144 00:09:16,290 --> 00:09:18,155 and also because the plateau stress 145 00:09:18,155 --> 00:09:20,200 is related to elastic buckling, it also 146 00:09:20,200 --> 00:09:22,820 depends on the modulus of the solid. 147 00:09:22,820 --> 00:09:27,010 So for elastomeric foams-- it's because you normalized it 148 00:09:27,010 --> 00:09:29,690 with respect to Es-- one of these diagrams 149 00:09:29,690 --> 00:09:32,487 will represent all elastomeric foams. 150 00:09:32,487 --> 00:09:34,070 So that's rather a nice thing-- so you 151 00:09:34,070 --> 00:09:35,960 can have different elastomeric foams, 152 00:09:35,960 --> 00:09:38,550 but one of those diagrams is going to represent all of them. 153 00:09:46,640 --> 00:09:49,730 So we can say, elastomeric foams can all 154 00:09:49,730 --> 00:09:53,030 be plotted on one plot, or one curve, 155 00:09:53,030 --> 00:09:55,275 since both the modulus and the plateau stress 156 00:09:55,275 --> 00:09:56,495 are related to Es. 157 00:10:38,390 --> 00:10:40,962 So if we look at this next figure here-- 158 00:10:40,962 --> 00:10:43,336 maybe I'll just wait a minute for people to stop writing. 159 00:10:50,060 --> 00:10:51,601 Some people write faster than others. 160 00:11:00,140 --> 00:11:02,230 So if we look at this next plot here, 161 00:11:02,230 --> 00:11:04,770 here's a compressive stress and strain. 162 00:11:04,770 --> 00:11:06,450 These tests are done for one density, 163 00:11:06,450 --> 00:11:08,283 but at different strain rates-- so it's kind 164 00:11:08,283 --> 00:11:10,170 of the other version of this. 165 00:11:10,170 --> 00:11:12,370 But here's the stress strain curves here, 166 00:11:12,370 --> 00:11:14,830 and here's the energy absorption diagram that's 167 00:11:14,830 --> 00:11:16,260 derived from those. 168 00:11:16,260 --> 00:11:19,580 And then here's a summary diagram 169 00:11:19,580 --> 00:11:22,210 that has the different strain rates, and that would 170 00:11:22,210 --> 00:11:24,130 have different densities here. 171 00:11:24,130 --> 00:11:26,220 And the idea is this diagram here 172 00:11:26,220 --> 00:11:28,870 could represent all elastomeric foams. 173 00:11:28,870 --> 00:11:31,090 So this has been put together for polyurethane, 174 00:11:31,090 --> 00:11:34,210 but it should be able to represent other sorts 175 00:11:34,210 --> 00:11:40,980 of flexible elastomeric foams. 176 00:11:40,980 --> 00:11:41,994 Sorry? 177 00:11:41,994 --> 00:11:44,602 AUDIENCE: In those diagrams, then, 178 00:11:44,602 --> 00:11:46,320 the intersection of this strain rate 179 00:11:46,320 --> 00:11:48,350 line and your relative density line 180 00:11:48,350 --> 00:11:50,330 should be the shoulder position? 181 00:11:50,330 --> 00:11:51,590 LORNA GIBSON: Yeah, exactly. 182 00:11:51,590 --> 00:11:56,520 And so this line here is for 0.01, and that one's for 0.03. 183 00:11:56,520 --> 00:11:58,370 So 0.02 is going to be-- you'd have 184 00:11:58,370 --> 00:12:01,530 to interpolate somewhere in between there. 185 00:12:01,530 --> 00:12:03,586 So we've just put on certain values, 186 00:12:03,586 --> 00:12:05,710 because we're not going to put on a million values. 187 00:12:05,710 --> 00:12:09,700 We just put on certain ones, and then you 188 00:12:09,700 --> 00:12:11,820 can estimate where other densities would 189 00:12:11,820 --> 00:12:12,840 appear on there. 190 00:12:12,840 --> 00:12:14,710 OK? 191 00:12:14,710 --> 00:12:17,430 So here's another example here-- these are 192 00:12:17,430 --> 00:12:19,020 curves for two different foams. 193 00:12:19,020 --> 00:12:21,130 So here's a polyurethane a polyethylene, 194 00:12:21,130 --> 00:12:22,790 so these are both elastomers. 195 00:12:22,790 --> 00:12:25,690 And one is the dashed line, and one is the solid line. 196 00:12:25,690 --> 00:12:28,530 And you can kind of see how the lines mesh up. 197 00:12:28,530 --> 00:12:32,970 So here's a density of 0.01 for the polyurethane. 198 00:12:32,970 --> 00:12:35,760 Here's 0.05 for the polyurethane. 199 00:12:35,760 --> 00:12:38,250 And here's 0.06 for the polyethylene. 200 00:12:38,250 --> 00:12:40,460 And you can see how the 0.06 and 0.05-- 201 00:12:40,460 --> 00:12:42,220 they're not quite on top of each other, 202 00:12:42,220 --> 00:12:44,553 but they're pretty close to coming on top of each other. 203 00:12:44,553 --> 00:12:47,910 And then 0.1, 0.12-- and so you get a family of them 204 00:12:47,910 --> 00:12:50,480 for the different densities. 205 00:12:50,480 --> 00:12:53,150 And you can also do this for materials 206 00:12:53,150 --> 00:12:56,500 that have a yield point, so polymethacrylimid has a yield 207 00:12:56,500 --> 00:12:59,940 point, so you do exactly the same kind of thing. 208 00:12:59,940 --> 00:13:01,840 So here's the energy absorption diagram 209 00:13:01,840 --> 00:13:04,480 that's been developed from the stress strain curves. 210 00:13:04,480 --> 00:13:07,870 But now this curve here, or this set of curves here, 211 00:13:07,870 --> 00:13:11,740 is really just valid for one ratio of sigma [? ys ?] 212 00:13:11,740 --> 00:13:15,996 to Es-- so the solid yield strength of the solid modulus. 213 00:13:15,996 --> 00:13:17,370 So it's valid for whatever it was 214 00:13:17,370 --> 00:13:24,230 for that particular type of foam-- the polymethacrylimid. 215 00:13:28,330 --> 00:13:35,200 So I'll just say, if we have foams 216 00:13:35,200 --> 00:13:37,846 that are made from a material with a yield point-- 217 00:13:37,846 --> 00:13:43,220 and so they have a plastic collapse stress-- then 218 00:13:43,220 --> 00:13:53,450 the curve will be valid for foams 219 00:13:53,450 --> 00:13:55,790 with the same ratio of [? sigma ys ?] to Es. 220 00:14:06,210 --> 00:14:09,730 So in that case there, for the polymethacrylimid, 221 00:14:09,730 --> 00:14:14,230 that ratio is about equal to 1 over 30. 222 00:14:14,230 --> 00:14:17,660 So that plot would probably give not a bad description 223 00:14:17,660 --> 00:14:24,860 of other foams, with the same value of sigma ys over Es. 224 00:14:24,860 --> 00:14:26,490 So the idea here is we can generate 225 00:14:26,490 --> 00:14:30,379 these diagrams either from data-- the way 226 00:14:30,379 --> 00:14:32,337 those ones have been done-- or from the models. 227 00:15:35,410 --> 00:15:39,130 So another way to generate these is to think about the models 228 00:15:39,130 --> 00:15:41,674 that we have for the foams, and the foam behavior. 229 00:15:41,674 --> 00:15:44,090 So we have an equation that describes the Young's modulus, 230 00:15:44,090 --> 00:15:46,880 we have equations that describe the plateau stresses, 231 00:15:46,880 --> 00:15:50,570 we have an empirical equation for the densification strain. 232 00:15:50,570 --> 00:15:53,500 And we can use those to generate these diagrams. 233 00:15:53,500 --> 00:15:55,180 And they're kind of useful, because they 234 00:15:55,180 --> 00:15:59,320 show you what's going on a sort of mechanistic basis. 235 00:15:59,320 --> 00:16:02,590 So this is a diagram here that's been generated for open cell 236 00:16:02,590 --> 00:16:04,140 elastomeric foams. 237 00:16:04,140 --> 00:16:06,050 Here's our energy absorbed, here's 238 00:16:06,050 --> 00:16:07,870 our peak stress down here. 239 00:16:07,870 --> 00:16:11,650 This little inset is sort of a schematic of the idealized foam 240 00:16:11,650 --> 00:16:12,150 behavior. 241 00:16:12,150 --> 00:16:13,790 So here's the Young's modulus, here's 242 00:16:13,790 --> 00:16:15,580 the elastic [? collapse ?] stress, here's 243 00:16:15,580 --> 00:16:17,770 the densification over here. 244 00:16:17,770 --> 00:16:21,480 So obviously it's kind of a very idealized set-up. 245 00:16:21,480 --> 00:16:23,274 But we can generate this diagram-- 246 00:16:23,274 --> 00:16:25,190 and I'm going to go through the equations that 247 00:16:25,190 --> 00:16:26,860 will let us do that. 248 00:16:26,860 --> 00:16:32,260 So one thing to note is here's the curves for each density. 249 00:16:32,260 --> 00:16:35,340 Here is this line that connects the shoulder points. 250 00:16:35,340 --> 00:16:37,050 There's a couple of other lines on here 251 00:16:37,050 --> 00:16:39,550 that I just wanted to mention something about. 252 00:16:39,550 --> 00:16:42,240 If you think about the densities-- like that's 0.01, 253 00:16:42,240 --> 00:16:44,430 this is 0.03, that's 0.1-- if you 254 00:16:44,430 --> 00:16:48,540 had a fully dense solid that was made of the same elastomer, 255 00:16:48,540 --> 00:16:51,040 you could plot the curve for that, 256 00:16:51,040 --> 00:16:52,890 and that is going to show up over here. 257 00:16:52,890 --> 00:16:54,580 So this is kind of an upper bound. 258 00:16:54,580 --> 00:16:57,520 It can't get any more from that. 259 00:16:57,520 --> 00:17:01,030 And we've also got a dotted line here, 260 00:17:01,030 --> 00:17:03,870 which takes into account fluid flow within the cells. 261 00:17:03,870 --> 00:17:05,901 So there can be some fluid flow, and because we 262 00:17:05,901 --> 00:17:08,359 haven't talked about that, we're not going to go into that. 263 00:17:08,359 --> 00:17:10,619 So we can just ignore that dotted line for now. 264 00:17:13,380 --> 00:17:18,690 So let me go through how we can do the modeling. 265 00:17:18,690 --> 00:17:21,030 So we're going to divide the stress strain curve up 266 00:17:21,030 --> 00:17:23,530 into bits, and I'm going to write equations 267 00:17:23,530 --> 00:17:26,300 for the energy absorbed for each bit. 268 00:17:26,300 --> 00:17:30,102 So we're going to start with a linear elastic behavior. 269 00:17:33,030 --> 00:17:37,860 And I'm going to-- let's see-- yeah, 270 00:17:37,860 --> 00:17:41,570 so let me just note here that this is the densification 271 00:17:41,570 --> 00:17:43,070 strain out here. 272 00:17:43,070 --> 00:17:45,650 And this strain, epsilon naught, corresponds 273 00:17:45,650 --> 00:17:48,870 to the strain at which we first reach the stress plateau. 274 00:17:48,870 --> 00:17:51,600 So here, for the linear elastic part, 275 00:17:51,600 --> 00:17:55,670 I'm going to say that the strain is less than that. 276 00:17:55,670 --> 00:17:57,940 So the strain is less than absolute naught. 277 00:17:57,940 --> 00:18:02,200 And then I can say, the energy absorbed-- 278 00:18:02,200 --> 00:18:03,700 so if you just remember from Hooke's 279 00:18:03,700 --> 00:18:06,830 law on linear elasticity, energy under the stress strain 280 00:18:06,830 --> 00:18:08,360 curve for the linear elastic part 281 00:18:08,360 --> 00:18:11,810 is 1/2 of sigma squared over E. So I'm 282 00:18:11,810 --> 00:18:14,510 going to call sigma-- whatever the stress is going to be, 283 00:18:14,510 --> 00:18:16,510 the peak stress that we get to. 284 00:18:16,510 --> 00:18:18,980 And now we're going to divide by E of the foam-- 285 00:18:18,980 --> 00:18:21,100 because these were our foams here. 286 00:18:21,100 --> 00:18:30,070 And I can use our model here to say-- 287 00:18:30,070 --> 00:18:31,740 and now I've got to divide that by Es, 288 00:18:31,740 --> 00:18:33,220 because I've normalized here. 289 00:18:40,680 --> 00:18:42,830 So because I know from my modeling 290 00:18:42,830 --> 00:18:44,850 that the Young's modulus of the foam 291 00:18:44,850 --> 00:18:47,500 is just equal to Es times the relative density squared 292 00:18:47,500 --> 00:18:49,390 for the open celled foam, that means 293 00:18:49,390 --> 00:18:52,230 I've now got an Es squared in the denominator, 294 00:18:52,230 --> 00:18:54,310 so I've got a sigma p over Es squared. 295 00:18:54,310 --> 00:18:59,790 And then I've got a 1 over the relative density squared term. 296 00:18:59,790 --> 00:19:04,610 So that factor there, that equation there, 297 00:19:04,610 --> 00:19:07,340 gives you these first set of lines here. 298 00:19:07,340 --> 00:19:10,370 Gives you that bit, and this bit, and that bit. 299 00:19:10,370 --> 00:19:13,143 So it gives you those first parts of the energy absorption 300 00:19:13,143 --> 00:19:13,643 diagram. 301 00:19:21,410 --> 00:19:23,810 And then if we look at the stress plateau-- 302 00:19:23,810 --> 00:19:27,300 so here we're going to say that epsilon naught is less 303 00:19:27,300 --> 00:19:30,940 than epsilon is less than the densification strain-- 304 00:19:30,940 --> 00:19:33,420 so we're on the plateau somewhere. 305 00:19:33,420 --> 00:19:36,560 And now the energy absorbed is just 306 00:19:36,560 --> 00:19:40,320 going to be our plateau stress times the amount of strain 307 00:19:40,320 --> 00:19:43,360 we've got. 308 00:19:43,360 --> 00:19:46,290 So that's epsilon minus epsilon naught. 309 00:19:46,290 --> 00:19:50,080 And if I normalized with respect the solid modulus, 310 00:19:50,080 --> 00:19:59,300 I can write down that my plateau stress is 0.05 times 311 00:19:59,300 --> 00:20:01,510 the relative density squared, and then 312 00:20:01,510 --> 00:20:05,125 multiply that times epsilon minus epsilon naught. 313 00:20:08,900 --> 00:20:11,000 So that equation then corresponds 314 00:20:11,000 --> 00:20:14,510 to these vertical parts-- so this part here, that part 315 00:20:14,510 --> 00:20:16,090 there, this part here. 316 00:20:16,090 --> 00:20:19,070 It corresponds to those vertical lines on the figure. 317 00:20:34,020 --> 00:20:36,090 Vertical lines on the diagram. 318 00:20:36,090 --> 00:20:38,110 And then the plateau stress is going 319 00:20:38,110 --> 00:20:40,490 to end at the densification strain. 320 00:20:45,830 --> 00:20:47,753 And at that point, the energy diagram 321 00:20:47,753 --> 00:20:49,128 is just going to become vertical. 322 00:21:37,120 --> 00:21:39,114 OK, and then the last part-- I'll 323 00:21:39,114 --> 00:21:40,613 try to rub this off a little better. 324 00:21:47,130 --> 00:21:48,870 And then the last part is when we're 325 00:21:48,870 --> 00:22:01,930 at the end of this stress plateau, 326 00:22:01,930 --> 00:22:06,180 and the strain is equal to that densification strain. 327 00:22:06,180 --> 00:22:08,360 And so the amount of energy we absorb here 328 00:22:08,360 --> 00:22:09,776 is really going to be the maximum. 329 00:22:35,504 --> 00:22:36,920 So this is the energy that's going 330 00:22:36,920 --> 00:22:38,740 to correspond to that shoulder point 331 00:22:38,740 --> 00:22:40,790 that I've been talking about. 332 00:22:40,790 --> 00:22:46,360 So I'm going to call that W max, and normalize that with respect 333 00:22:46,360 --> 00:22:47,810 to Es. 334 00:22:47,810 --> 00:22:52,800 And that's then going to be our plateau stress 335 00:22:52,800 --> 00:22:56,960 times the densification strain. 336 00:22:56,960 --> 00:23:02,246 And the densification strain was just 1 minus 1.4 times 337 00:23:02,246 --> 00:23:03,120 the relative density. 338 00:23:11,330 --> 00:23:17,780 So here I'm assuming that the densification strain 339 00:23:17,780 --> 00:23:20,580 is very much bigger than the strain at which 340 00:23:20,580 --> 00:23:23,000 the buckling first occurs, and I'm neglecting 341 00:23:23,000 --> 00:23:24,415 that linear elastic part. 342 00:23:34,800 --> 00:23:39,890 So then we could say that the optimum foam 343 00:23:39,890 --> 00:23:41,860 is at that shoulder point. 344 00:23:54,880 --> 00:23:57,020 And I can say that the peak stress at that point 345 00:23:57,020 --> 00:23:58,933 is just equal to the plateau stress. 346 00:24:03,370 --> 00:24:08,590 And what I want to do is get an equation for that solid line 347 00:24:08,590 --> 00:24:11,430 up here that connects all those shoulder points. 348 00:24:11,430 --> 00:24:13,780 So I want an equation, in terms of the energy, 349 00:24:13,780 --> 00:24:16,700 and the peak stress, instead of in terms of the density. 350 00:24:16,700 --> 00:24:19,130 So what I'm going to do a solve this for the density, 351 00:24:19,130 --> 00:24:20,867 and then plug that back into there. 352 00:24:34,287 --> 00:24:36,120 So I get that the relative density is, then, 353 00:24:36,120 --> 00:24:40,067 20 times the peak stress over the solid modulus, 354 00:24:40,067 --> 00:24:41,525 and I take the square root of that. 355 00:24:49,600 --> 00:24:54,612 And now I can substitute this up here for the relative density. 356 00:24:54,612 --> 00:24:55,820 I think I need another board. 357 00:25:29,710 --> 00:25:32,680 So then I've got-- this is my peak stress, or my plateau 358 00:25:32,680 --> 00:25:39,670 stress, over Es, and this is all just the densification strain. 359 00:25:39,670 --> 00:25:42,454 And that's just 1 minus 1.4 times the relative density. 360 00:25:42,454 --> 00:25:44,120 But now I'm putting the relative density 361 00:25:44,120 --> 00:25:47,085 in terms of the peak stress, or the plateau stress. 362 00:25:57,290 --> 00:26:00,830 If I just simplify that slightly with the constant, 363 00:26:00,830 --> 00:26:08,312 it's 1 minus 6.26 times sigma p over Es to the 1/2 power. 364 00:26:11,930 --> 00:26:18,270 So that equation there describes the-- oops, no more updates. 365 00:26:18,270 --> 00:26:19,390 No updates. 366 00:26:19,390 --> 00:26:21,494 Go away. 367 00:26:21,494 --> 00:26:25,870 Ah, so that equation there describes this line here that 368 00:26:25,870 --> 00:26:28,367 connects those shoulder points. 369 00:26:28,367 --> 00:26:30,450 And that's the line you're the most interested in, 370 00:26:30,450 --> 00:26:32,250 because each of those shoulder points 371 00:26:32,250 --> 00:26:34,100 is a point where the foam is being 372 00:26:34,100 --> 00:26:37,355 used in the most efficient way, or the optimum way. 373 00:26:48,509 --> 00:26:50,300 And then, let's see-- is that going to fit? 374 00:26:50,300 --> 00:26:51,714 No-- let me try the other board. 375 00:26:55,505 --> 00:26:56,880 And then the last thing we can do 376 00:26:56,880 --> 00:26:59,910 is calculate that line that corresponds to the dense solid. 377 00:26:59,910 --> 00:27:02,072 Yeah? 378 00:27:02,072 --> 00:27:04,055 AUDIENCE: On those ones over there, 379 00:27:04,055 --> 00:27:06,554 it says it corresponds to the vertical lines on the diagram. 380 00:27:06,554 --> 00:27:08,554 And then later it says then it becomes vertical. 381 00:27:08,554 --> 00:27:11,050 Is that referring to two different diagrams? 382 00:27:11,050 --> 00:27:14,020 LORNA GIBSON: So this stress plateau equation 383 00:27:14,020 --> 00:27:18,320 here corresponds to these vertical lines here. 384 00:27:18,320 --> 00:27:23,220 So for relative density of 0.01, it corresponds to that part. 385 00:27:23,220 --> 00:27:25,340 For 0.03 it's this part. 386 00:27:25,340 --> 00:27:27,560 And your 0.01 it's that part. 387 00:27:27,560 --> 00:27:29,522 AUDIENCE: But then some of the [INAUDIBLE] 388 00:27:29,522 --> 00:27:32,246 it says, then w [? versus ?] sigma becomes vertical. 389 00:27:32,246 --> 00:27:33,400 Should that-- 390 00:27:33,400 --> 00:27:35,120 LORNA GIBSON: So, well the plateau stress 391 00:27:35,120 --> 00:27:36,920 ends at the densification strain. 392 00:27:36,920 --> 00:27:39,200 So the plateau stress ends here. 393 00:27:39,200 --> 00:27:41,810 Oh, let's see-- and then it becomes-- should be horizontal. 394 00:27:41,810 --> 00:27:42,310 Sorry. 395 00:27:56,850 --> 00:27:58,140 OK, sorry. 396 00:27:58,140 --> 00:27:58,640 Happy? 397 00:28:01,657 --> 00:28:03,240 And now I'm going to rub that all off. 398 00:28:15,230 --> 00:28:16,560 OK, did everybody get this? 399 00:28:16,560 --> 00:28:17,268 I can rub it off? 400 00:28:36,050 --> 00:28:45,350 OK, so then the last part is what happens 401 00:28:45,350 --> 00:28:48,540 when the foam is densified. 402 00:28:48,540 --> 00:28:50,540 And if it was fully dense-- and you never really 403 00:28:50,540 --> 00:28:52,200 can get to this point-- but if it was fully dense, 404 00:28:52,200 --> 00:28:53,658 you would get rid of all the pores, 405 00:28:53,658 --> 00:28:55,040 and it would just be a solid. 406 00:28:55,040 --> 00:28:56,750 And then the energy absorption curve 407 00:28:56,750 --> 00:29:00,200 would be the curve for the solid. 408 00:29:00,200 --> 00:29:09,142 So I'll just say, when fully densified, 409 00:29:09,142 --> 00:29:13,095 I'm going to say a curve approaches that for the solid. 410 00:29:19,450 --> 00:29:24,695 And for the solid, you would just have that W over Es 411 00:29:24,695 --> 00:29:29,885 is equal to 1/2 the peak stress squared over Es. 412 00:29:33,410 --> 00:29:36,650 So this model curve, the curves have the same shape 413 00:29:36,650 --> 00:29:40,070 as when you get the diagrams from the experiments. 414 00:29:40,070 --> 00:29:42,190 And you can see how the different mechanisms 415 00:29:42,190 --> 00:29:45,422 of deformation and failure contribute to the diagram, 416 00:29:45,422 --> 00:29:46,630 where the diagram comes from. 417 00:29:48,884 --> 00:29:50,300 And I guess one other point is you 418 00:29:50,300 --> 00:29:53,120 can see that the foams are always going to be a lot better 419 00:29:53,120 --> 00:29:54,260 than the solid. 420 00:29:54,260 --> 00:29:56,050 And remember this is a log log curve, 421 00:29:56,050 --> 00:30:01,010 so that a foam that has a density of 3% here, there's 422 00:30:01,010 --> 00:30:03,460 a huge difference in the peak stress. 423 00:30:03,460 --> 00:30:07,740 So say you wanted to absorb this amount of energy up here, 424 00:30:07,740 --> 00:30:10,640 for a foam that was 0.03 dense, the peak stress 425 00:30:10,640 --> 00:30:13,900 would be a little less than 10 to the minus 4, 426 00:30:13,900 --> 00:30:15,520 normalized by the modulus. 427 00:30:15,520 --> 00:30:17,870 And for the solid, it would be 10 to the minus 2-- 428 00:30:17,870 --> 00:30:19,630 so it's orders of magnitude better to have 429 00:30:19,630 --> 00:30:23,040 the foam rather than the solid. 430 00:30:23,040 --> 00:30:27,030 All right, now let's see what else we have. 431 00:30:27,030 --> 00:30:29,890 So we could do a similar thing for closed-cell foams, 432 00:30:29,890 --> 00:30:32,066 and you get diagrams that look like this. 433 00:30:32,066 --> 00:30:34,440 One of the differences with the closed-cell foams, if you 434 00:30:34,440 --> 00:30:37,950 assume that the faces don't rupture, the plateau stresses 435 00:30:37,950 --> 00:30:41,160 and horizontals-- remember we had that gas contribution, 436 00:30:41,160 --> 00:30:43,270 and you can take that into account? 437 00:30:43,270 --> 00:30:46,410 So I'm not going to go over the details of that. 438 00:30:46,410 --> 00:30:47,960 The next one I wanted to talk about 439 00:30:47,960 --> 00:30:51,500 was looking at foams that have a yield point. 440 00:30:51,500 --> 00:30:54,200 And again, you can generate a similar kind of diagram, 441 00:30:54,200 --> 00:30:57,480 but now, instead of having an elastic failure here, 442 00:30:57,480 --> 00:31:00,810 you've got a plastic failure-- you form plastic hinges. 443 00:31:00,810 --> 00:31:02,670 And then again, this diagram is less 444 00:31:02,670 --> 00:31:06,000 general than the one for elastomeric foams, 445 00:31:06,000 --> 00:31:10,150 so this diagram would be valid for whatever ratio of sigma ys 446 00:31:10,150 --> 00:31:11,810 over Es you've the calculation for. 447 00:31:11,810 --> 00:31:14,730 So this one here is for 0.01. 448 00:31:14,730 --> 00:31:17,590 So let me just run through the same kind of calculation 449 00:31:17,590 --> 00:31:19,930 for the plastic foams. 450 00:31:25,414 --> 00:31:26,830 Can I rub this off, and then I can 451 00:31:26,830 --> 00:31:28,280 use this board to start here? 452 00:32:01,960 --> 00:32:07,980 OK, so the linear elastic part is just the same 453 00:32:07,980 --> 00:32:10,970 as for the elastomeric foams. 454 00:32:10,970 --> 00:32:16,956 So you get W over Es is 1/2. 455 00:32:16,956 --> 00:32:21,970 Sigma p over Es squared times 1 over the relative density 456 00:32:21,970 --> 00:32:24,700 squared, so it's just the same thing. 457 00:32:24,700 --> 00:32:34,370 And the stress plateau-- you get w over Es 458 00:32:34,370 --> 00:32:43,010 is just the plastic collapse strength times the strain range 459 00:32:43,010 --> 00:32:44,960 that you go up to. 460 00:32:44,960 --> 00:32:46,980 So if you remember the plastic collapse strength 461 00:32:46,980 --> 00:32:55,260 was 0.3 sigma ys times the relative density to the 3/2 462 00:32:55,260 --> 00:32:57,590 power, and then times the strain range. 463 00:33:06,820 --> 00:33:09,290 And then at the end of the stress plateau, 464 00:33:09,290 --> 00:33:13,310 you've got the maximum energy absorbed. 465 00:33:13,310 --> 00:33:16,420 So normalize that by Es. 466 00:33:16,420 --> 00:33:20,300 And that's going to be your peak stress over Es 467 00:33:20,300 --> 00:33:22,395 times the densification strain again. 468 00:33:26,870 --> 00:33:31,674 So this bit here is the densification strain. 469 00:33:37,000 --> 00:33:38,530 And then you can do a similar thing 470 00:33:38,530 --> 00:33:40,363 to figure out the equation of that line that 471 00:33:40,363 --> 00:33:41,590 joins the shoulder points. 472 00:34:04,220 --> 00:34:08,155 So the first step is to solve for the relative density there. 473 00:34:24,130 --> 00:34:27,810 So if this part here-- 0.3 sigma ys times the relative density 474 00:34:27,810 --> 00:34:31,719 to the 3/2 power is the plastic collapse stress, 475 00:34:31,719 --> 00:34:35,760 then at the densification point, the relative density, 476 00:34:35,760 --> 00:34:38,690 you just rewrite that and it comes out to the 2/3 power, 477 00:34:38,690 --> 00:34:40,580 because you turn the power around. 478 00:34:40,580 --> 00:34:42,870 And then you just substitute this up in here. 479 00:35:17,280 --> 00:35:20,070 So you get that the maximum energy absorbed, 480 00:35:20,070 --> 00:35:23,310 normalized by the solid modulus, is your peak stress, times 481 00:35:23,310 --> 00:35:27,290 1 minus 1.4 times this thing in brackets to the 2/3 power-- 482 00:35:27,290 --> 00:35:30,350 the 3.3 times the peak stress over the yield 483 00:35:30,350 --> 00:35:31,930 strength of the solid. 484 00:35:31,930 --> 00:35:40,830 And then if I just rearrange that, and get the constants, 485 00:35:40,830 --> 00:35:51,890 it's 1 minus 3.1 times our ratio of the stresses there. 486 00:35:57,060 --> 00:35:59,610 So maybe I'll just put over here-- 487 00:35:59,610 --> 00:36:04,465 the curves are less general than for elastomeric foams. 488 00:36:31,100 --> 00:36:33,280 So each family of curves would be 489 00:36:33,280 --> 00:36:36,400 for a particular ratio of the solid yield strength 490 00:36:36,400 --> 00:36:37,453 to the solid modulus. 491 00:37:22,590 --> 00:37:23,490 So you get the idea? 492 00:37:23,490 --> 00:37:25,880 It's fairly straightforward. 493 00:37:25,880 --> 00:37:27,690 So I wanted to finish up this topic 494 00:37:27,690 --> 00:37:31,280 by giving you a few examples of how you can use these curves. 495 00:37:31,280 --> 00:37:33,560 So the next thing is to look at the selection of foams 496 00:37:33,560 --> 00:37:35,080 for impact protection. 497 00:37:35,080 --> 00:37:37,750 And typically, you're given some information about the objects-- 498 00:37:37,750 --> 00:37:39,850 so typically you want to protect some object. 499 00:37:39,850 --> 00:37:42,230 It could be a computer, it could be your head, 500 00:37:42,230 --> 00:37:43,650 some part of your body. 501 00:37:43,650 --> 00:37:45,650 So typically you know something about the object 502 00:37:45,650 --> 00:37:46,680 you want to protect. 503 00:37:46,680 --> 00:37:50,350 So you might know its mass, you might know the area of contact, 504 00:37:50,350 --> 00:37:52,280 you might say, well, if it's my computer, 505 00:37:52,280 --> 00:37:53,890 I want to make sure it doesn't break if I drop it 506 00:37:53,890 --> 00:37:54,890 from a height of a meter. 507 00:37:54,890 --> 00:37:56,550 Or you could say whatever, [? maybe it's ?] 2 meters. 508 00:37:56,550 --> 00:37:58,010 But you pick something. 509 00:37:58,010 --> 00:37:59,820 And so there's a certain amount of energy 510 00:37:59,820 --> 00:38:01,410 you know that you need to absorb. 511 00:38:01,410 --> 00:38:04,310 And you may know that whatever the component is, 512 00:38:04,310 --> 00:38:06,280 or the body part, or whatever-- there's 513 00:38:06,280 --> 00:38:09,427 some maximum acceleration you can tolerate. 514 00:38:09,427 --> 00:38:11,010 So you might say, well, I want to make 515 00:38:11,010 --> 00:38:14,180 sure my computer doesn't break under acceleration of so much. 516 00:38:14,180 --> 00:38:16,399 So you're given the acceleration. 517 00:38:16,399 --> 00:38:18,440 And so if you know the mass and the acceleration, 518 00:38:18,440 --> 00:38:19,814 and you know the area of contact, 519 00:38:19,814 --> 00:38:22,300 you can figure out a force over an area, 520 00:38:22,300 --> 00:38:24,140 and that gives you the peak stress. 521 00:38:24,140 --> 00:38:26,940 So typically, you know those things in the problem. 522 00:38:26,940 --> 00:38:29,700 And typically the problem involves choosing a material, 523 00:38:29,700 --> 00:38:31,810 or choosing-- like choosing what kind of material 524 00:38:31,810 --> 00:38:34,390 do you want to make the foam out of, and what density of foam 525 00:38:34,390 --> 00:38:35,800 do you want to use, what thickness of foam 526 00:38:35,800 --> 00:38:36,810 do you want to use? 527 00:38:36,810 --> 00:38:38,830 So I've got a couple of examples just 528 00:38:38,830 --> 00:38:40,580 to show you how this works. 529 00:38:40,580 --> 00:38:43,094 So let me just write down a couple notes, and then 530 00:38:43,094 --> 00:38:45,677 the rest of it I think I'm just going to take from the slides. 531 00:39:09,140 --> 00:39:12,410 So typically, you know what it is you want to protect, 532 00:39:12,410 --> 00:39:13,850 and you know something about it. 533 00:39:20,714 --> 00:39:22,380 So if you know what it is, typically you 534 00:39:22,380 --> 00:39:23,557 know what the mass is. 535 00:39:28,700 --> 00:39:31,090 You might know what the contact area would be. 536 00:39:41,300 --> 00:39:49,279 Say a maximum drop height, maximum tolerable acceleration. 537 00:39:53,870 --> 00:39:55,750 So say if you're worried about brain injury-- 538 00:39:55,750 --> 00:39:59,230 and making a helmet-- you might know what the maximum tolerable 539 00:39:59,230 --> 00:40:00,482 acceleration would be. 540 00:40:06,870 --> 00:40:09,720 So typically, you know what the peak allowable stress is, just 541 00:40:09,720 --> 00:40:11,770 from whatever the object itself is. 542 00:40:11,770 --> 00:40:15,700 And the variables that you have to play around 543 00:40:15,700 --> 00:40:25,530 with-- variables-- are things like the foam material, 544 00:40:25,530 --> 00:40:28,965 the foam density, and the foam thickness. 545 00:40:32,420 --> 00:40:34,030 So I have a couple of examples that 546 00:40:34,030 --> 00:40:37,910 have different setups here. 547 00:40:37,910 --> 00:40:41,610 And we'll just see how the thing works out here. 548 00:40:41,610 --> 00:40:45,520 So the first example, we're told the mass of the packaged object 549 00:40:45,520 --> 00:40:47,210 is 1/2 kilogram. 550 00:40:47,210 --> 00:40:49,870 We're told the area of contact between the foam 551 00:40:49,870 --> 00:40:51,370 and the object is going to be point. 552 00:40:51,370 --> 00:40:53,190 0.01 of 1 meter squared. 553 00:40:53,190 --> 00:40:54,700 And we're told that it's supposed 554 00:40:54,700 --> 00:40:57,830 to be designed to withstand a drop of 1 meter-- 555 00:40:57,830 --> 00:40:59,790 so if the drop height is 1 meter, 556 00:40:59,790 --> 00:41:03,670 then the velocity is just the square root of 2gh. 557 00:41:03,670 --> 00:41:06,620 So g is gravity, so you can work out the velocity on impact 558 00:41:06,620 --> 00:41:09,184 would be 4.5 meters per second. 559 00:41:09,184 --> 00:41:11,350 And if you have the velocity on impact and the mass, 560 00:41:11,350 --> 00:41:13,387 you can figure out the energy to be absorbed. 561 00:41:13,387 --> 00:41:14,970 You can say mv squared screwed over 2, 562 00:41:14,970 --> 00:41:17,280 or you could say it's mgh-- either way. 563 00:41:17,280 --> 00:41:20,430 So here it's going to work out to 5 joules. 564 00:41:20,430 --> 00:41:25,100 And in this case, we're told that the maximum deceleration 565 00:41:25,100 --> 00:41:29,300 is 10g-- so then if that's 10g, the maximum force is the mass 566 00:41:29,300 --> 00:41:30,900 times the acceleration. 567 00:41:30,900 --> 00:41:32,920 That works out to 50 Newtons. 568 00:41:32,920 --> 00:41:34,800 And then that gives us a peak stress, 569 00:41:34,800 --> 00:41:36,240 the maximum allowable peak stress 570 00:41:36,240 --> 00:41:39,060 of the force over the area it's 5 kiloNewtons per meter 571 00:41:39,060 --> 00:41:40,270 squared. 572 00:41:40,270 --> 00:41:42,240 And in this case, we're told that the foam is 573 00:41:42,240 --> 00:41:44,400 going to be a flexible polyurethane, 574 00:41:44,400 --> 00:41:47,550 and it has a solid modulus of 50 megapascals. 575 00:41:47,550 --> 00:41:49,920 And so we can calculate this normalized peak stress. 576 00:41:49,920 --> 00:41:53,110 So the normalized peak stress here is 10 to the minus 4. 577 00:41:53,110 --> 00:41:56,350 So in this problem here, we need to figure out 578 00:41:56,350 --> 00:41:58,020 what's the foam density, and what's 579 00:41:58,020 --> 00:42:01,450 the thickness of the foam to protect the object? 580 00:42:01,450 --> 00:42:05,024 And so that last slide is just summarized here. 581 00:42:05,024 --> 00:42:07,190 And I realized that when I was going to put this up, 582 00:42:07,190 --> 00:42:08,773 the font is going to be kind of small, 583 00:42:08,773 --> 00:42:10,680 so I blew it up a little. 584 00:42:10,680 --> 00:42:12,980 So we have figured out that we're 585 00:42:12,980 --> 00:42:15,850 at sigma p over Es-- the peak stress normalized 586 00:42:15,850 --> 00:42:18,372 by the solid modulus is 10 to the minus 4. 587 00:42:18,372 --> 00:42:19,830 And we know that we're going to use 588 00:42:19,830 --> 00:42:22,840 a flexible elastomeric polyurethane, 589 00:42:22,840 --> 00:42:26,330 so we pull out our diagram for elastomeric foams. 590 00:42:26,330 --> 00:42:28,660 And this sort of hashed band here 591 00:42:28,660 --> 00:42:30,940 corresponds to all the different strain rates, and all 592 00:42:30,940 --> 00:42:31,990 the different densities. 593 00:42:31,990 --> 00:42:33,900 So I haven't plotted each individual line, 594 00:42:33,900 --> 00:42:37,970 we've just got this band that represents the whole thing. 595 00:42:37,970 --> 00:42:39,510 So we know that our normalized peak 596 00:42:39,510 --> 00:42:43,060 stress is going to be somewhere along this line here. 597 00:42:43,060 --> 00:42:44,620 That's from everything that's given, 598 00:42:44,620 --> 00:42:46,220 and what we can calculate. 599 00:42:46,220 --> 00:42:48,220 And we want to know what density of foam to use, 600 00:42:48,220 --> 00:42:49,610 and what thickness. 601 00:42:49,610 --> 00:42:52,300 So the way you approach this is the thickness 602 00:42:52,300 --> 00:42:53,759 is going to affect the strain rate. 603 00:42:53,759 --> 00:42:56,299 So the strain rate's just going to be the velocity on impact, 604 00:42:56,299 --> 00:42:58,590 divided by the thickness-- or it's an approximation 605 00:42:58,590 --> 00:42:59,960 for the strain rate. 606 00:42:59,960 --> 00:43:02,380 So we don't know if we're at this point down here, 607 00:43:02,380 --> 00:43:03,950 or if we're at this point up there, 608 00:43:03,950 --> 00:43:06,190 because we don't know where we are in the strain rate 609 00:43:06,190 --> 00:43:07,580 end of things. 610 00:43:07,580 --> 00:43:10,506 So the way you solve this is you just guess a thickness. 611 00:43:10,506 --> 00:43:11,880 And if you guess a thickness, you 612 00:43:11,880 --> 00:43:13,237 can calculate a strain rate. 613 00:43:13,237 --> 00:43:14,820 Then if you calculate the strain rate, 614 00:43:14,820 --> 00:43:16,650 you know where in this band you are. 615 00:43:16,650 --> 00:43:19,370 You can figure out a value of W over Es. 616 00:43:19,370 --> 00:43:21,970 And you can use an iterative process. 617 00:43:21,970 --> 00:43:23,690 And the way this is set up is we've 618 00:43:23,690 --> 00:43:27,090 chosen two very different initial thicknesses, 619 00:43:27,090 --> 00:43:29,130 and the point of doing that is to show you 620 00:43:29,130 --> 00:43:31,190 that it converges very quickly. 621 00:43:31,190 --> 00:43:33,410 So the first iteration on this side 622 00:43:33,410 --> 00:43:35,540 here, we've chosen the thickness of a meter, which 623 00:43:35,540 --> 00:43:38,590 is probably unlikely that we need a meter of foam. 624 00:43:38,590 --> 00:43:41,450 And on the side here, we've chosen a millimeter-- 0.001 625 00:43:41,450 --> 00:43:41,950 meters. 626 00:43:41,950 --> 00:43:43,620 So probably, we need more than that. 627 00:43:43,620 --> 00:43:45,078 So we probably need to be somewhere 628 00:43:45,078 --> 00:43:46,570 between those two bounds. 629 00:43:46,570 --> 00:43:49,600 So if the thickness was a meter, then the strain rate 630 00:43:49,600 --> 00:43:52,300 turns out to be 4.5 per second. 631 00:43:52,300 --> 00:43:54,940 And then we know where we are in this diagram, 632 00:43:54,940 --> 00:43:57,970 and we can read off a value of W over Es. 633 00:43:57,970 --> 00:44:00,350 So we know we're on this line here, 634 00:44:00,350 --> 00:44:02,220 and for a particular strain rate, 635 00:44:02,220 --> 00:44:04,580 we can read off the W over Es. 636 00:44:04,580 --> 00:44:08,660 So here's the value-- 5.25 times 10 to the minus 5. 637 00:44:08,660 --> 00:44:10,840 And if we know Es, which we do, we 638 00:44:10,840 --> 00:44:13,579 can then calculate the actual energy 639 00:44:13,579 --> 00:44:14,620 absorbed per unit volume. 640 00:44:14,620 --> 00:44:19,190 We get W-- so W is [? 2620 ?] joules per cubic meter. 641 00:44:19,190 --> 00:44:21,550 And we can use that value-- because that's 642 00:44:21,550 --> 00:44:24,904 an energy per unit volume-- we know the area of contact, 643 00:44:24,904 --> 00:44:27,320 and we can use that to get another value of the thickness. 644 00:44:27,320 --> 00:44:30,160 So we use that to calculate the next iteration 645 00:44:30,160 --> 00:44:31,580 of the thickness. 646 00:44:31,580 --> 00:44:34,190 So U is the total energy in joules, 647 00:44:34,190 --> 00:44:36,600 and W is the energy per unit volume. 648 00:44:36,600 --> 00:44:38,930 So U, the energy in joules, is going 649 00:44:38,930 --> 00:44:41,410 to equal the energy unit volume times the area 650 00:44:41,410 --> 00:44:42,746 times the thickness. 651 00:44:42,746 --> 00:44:44,120 So we know what the area is, too. 652 00:44:44,120 --> 00:44:46,270 We can then calculate a new thickness. 653 00:44:46,270 --> 00:44:49,320 So now our new thickness is 0.19 meters. 654 00:44:49,320 --> 00:44:50,790 We can use that to get a new strain 655 00:44:50,790 --> 00:44:53,790 rate-- that's 24 per second, and go through the whole thing 656 00:44:53,790 --> 00:44:54,390 again. 657 00:44:54,390 --> 00:44:58,320 And we end up with a revised energy of 3,300 joules 658 00:44:58,320 --> 00:45:00,032 per cubic meter. 659 00:45:00,032 --> 00:45:01,490 Now if we started at the other end, 660 00:45:01,490 --> 00:45:05,410 if we started with the first guess was a millimeter, then 661 00:45:05,410 --> 00:45:09,890 the strain rate is 4.5 times 10 to the minus 3 per second. 662 00:45:09,890 --> 00:45:12,270 That gives us a different value that we read off here 663 00:45:12,270 --> 00:45:15,780 for W over Es, and a different value for W. 664 00:45:15,780 --> 00:45:17,950 And then we use this value here for W 665 00:45:17,950 --> 00:45:20,230 to make another guess for the thickness. 666 00:45:20,230 --> 00:45:22,707 So that value is 0.14. 667 00:45:22,707 --> 00:45:24,290 And then we go through the whole thing 668 00:45:24,290 --> 00:45:27,580 again-- we get a revised strain rate a revised W over Es, 669 00:45:27,580 --> 00:45:31,510 and a revised W. And you can see after just two iterations, 670 00:45:31,510 --> 00:45:33,449 these two things are almost exactly the same. 671 00:45:33,449 --> 00:45:34,990 And then on the third iteration, they 672 00:45:34,990 --> 00:45:38,730 both would give you a thickness of point 0.15 meters. 673 00:45:38,730 --> 00:45:42,620 So even though you can pick wildly wrong first iterations, 674 00:45:42,620 --> 00:45:46,120 it converges very quickly, and it's a fairly simple 675 00:45:46,120 --> 00:45:48,310 calculation to do. 676 00:45:48,310 --> 00:45:51,210 So you know the thickness that you want is in here, 677 00:45:51,210 --> 00:45:54,180 and then you can get the optimum density here. 678 00:45:54,180 --> 00:45:58,540 So you know that your sigma p over Es is along this line 679 00:45:58,540 --> 00:46:00,970 of 10 to the minus 4--we're somewhere in here. 680 00:46:00,970 --> 00:46:03,210 These two strain rates here-- one was 24, 681 00:46:03,210 --> 00:46:06,400 one was 32-- so the final value is going 682 00:46:06,400 --> 00:46:08,210 to be somewhere around 30. 683 00:46:08,210 --> 00:46:10,550 And if you look on this thing here, 684 00:46:10,550 --> 00:46:12,830 you can see there's a line that corresponds to 10, 685 00:46:12,830 --> 00:46:14,624 there's a line that corresponds to 100. 686 00:46:14,624 --> 00:46:16,290 We're going to be right around in there. 687 00:46:16,290 --> 00:46:20,180 So the relative density is going to be right around 0.01. 688 00:46:20,180 --> 00:46:22,280 So you can use the diagram to get the thickness 689 00:46:22,280 --> 00:46:24,660 and to get the density. 690 00:46:24,660 --> 00:46:26,220 OK, are we good? 691 00:46:26,220 --> 00:46:28,320 We're good? 692 00:46:28,320 --> 00:46:31,190 So I've written some notes, and I'll just scan those 693 00:46:31,190 --> 00:46:34,370 and I'll put them in the Stellar site. 694 00:46:34,370 --> 00:46:37,700 So here's another example here-- and in this example, 695 00:46:37,700 --> 00:46:40,190 it's set up a little bit differently. 696 00:46:40,190 --> 00:46:44,212 So in this example here, we're not told the material, 697 00:46:44,212 --> 00:46:45,920 but we're told the thickness of the foam. 698 00:46:45,920 --> 00:46:47,910 So this time we want to get the material, 699 00:46:47,910 --> 00:46:50,460 and we want to get the density of the foam. 700 00:46:50,460 --> 00:46:53,020 So here we've got the specification. 701 00:46:53,020 --> 00:46:55,920 We're told the mass is 2 and 1/2 kilograms. 702 00:46:55,920 --> 00:46:58,724 The area of contact is 0.025 meters squared. 703 00:46:58,724 --> 00:47:01,224 We're told the thickness-- here thickness is 20 millimeters. 704 00:47:02,540 --> 00:47:04,844 We've got a drop height of 1 meter again. 705 00:47:04,844 --> 00:47:06,260 And the velocity of impact is then 706 00:47:06,260 --> 00:47:08,784 going to be 4.5 meters per second again. 707 00:47:08,784 --> 00:47:11,200 And since we know T, we know that the strain rate is going 708 00:47:11,200 --> 00:47:15,960 to be around 225 per second. 709 00:47:15,960 --> 00:47:19,700 We can calculate the energy absorbed-- [? MGH-- ?] 710 00:47:19,700 --> 00:47:21,790 25 joules. 711 00:47:21,790 --> 00:47:24,154 We can calculate the energy absorbed per unit volume, 712 00:47:24,154 --> 00:47:26,070 because we've got the area and the thickness-- 713 00:47:26,070 --> 00:47:28,694 so I'm just going to divide that by the area and the thickness. 714 00:47:28,694 --> 00:47:33,300 Now we have 5 times 10 to the 4th joules per cubic meter. 715 00:47:33,300 --> 00:47:35,520 And we're told that we're supposed to design it 716 00:47:35,520 --> 00:47:40,260 so the package can withstand a deceleration of 100g-- 717 00:47:40,260 --> 00:47:42,530 and so that gives you a maximum force. 718 00:47:42,530 --> 00:47:45,520 And here we've got a maximum allowable peak stress of 10 719 00:47:45,520 --> 00:47:48,460 of the 5 Newtons per meter squared. 720 00:47:48,460 --> 00:47:51,327 So here we have our curve for the elastomeric foams again-- 721 00:47:51,327 --> 00:47:53,410 let's assume it's going to be an elastomeric foam, 722 00:47:53,410 --> 00:47:56,290 but we don't know what kind of foam. 723 00:47:56,290 --> 00:47:58,180 So the way you solve this problem 724 00:47:58,180 --> 00:48:01,050 is that you make a guess for what Es is. 725 00:48:01,050 --> 00:48:04,480 So remember, these diagrams are all normalized by Es. 726 00:48:04,480 --> 00:48:07,630 So to plot a point on there, we need to know what Es is. 727 00:48:07,630 --> 00:48:09,440 So here, we're going to make a guess, 728 00:48:09,440 --> 00:48:13,850 and we're going to assume that Es is 100 megapascals to start. 729 00:48:13,850 --> 00:48:17,670 And if we had that value of Es, we know W, up here, 730 00:48:17,670 --> 00:48:19,700 and we know sigma p there. 731 00:48:19,700 --> 00:48:22,960 So we just divide those values of W and sigma p by Es, 732 00:48:22,960 --> 00:48:24,990 and we get these two values here. 733 00:48:24,990 --> 00:48:28,200 And we plot those two values on the thing here. 734 00:48:28,200 --> 00:48:30,450 So here's our point A-- and that corresponds 735 00:48:30,450 --> 00:48:33,300 to that first guess of 100 mega Pascals 736 00:48:33,300 --> 00:48:36,010 for the modulus of the solid. 737 00:48:36,010 --> 00:48:38,200 So that's not necessarily the final answer, 738 00:48:38,200 --> 00:48:41,210 that's not the right answer-- that's just somewhere to start. 739 00:48:41,210 --> 00:48:44,877 So the thing to notice is, if we have that point there, 740 00:48:44,877 --> 00:48:46,960 the strain rate there is probably not quite right. 741 00:48:46,960 --> 00:48:50,580 This upper bound here is-- let's see. 742 00:48:50,580 --> 00:48:51,790 Got to get closer. 743 00:48:51,790 --> 00:48:54,770 Oh, let's see-- that's 10 to the minus 2, that's 10 to the 2. 744 00:48:54,770 --> 00:48:57,280 So the strain rate we want to be is closer up to here, 745 00:48:57,280 --> 00:48:59,830 it's not quite down there. 746 00:48:59,830 --> 00:49:02,240 So we're not at the right strain rate. 747 00:49:02,240 --> 00:49:05,650 But the thing to notice is that if we draw a line of slope 1-- 748 00:49:05,650 --> 00:49:08,090 so there's this dash line of slope 1-- 749 00:49:08,090 --> 00:49:11,895 when we move up and down that line, we're just changing Es. 750 00:49:11,895 --> 00:49:13,770 Because everything is normalized with respect 751 00:49:13,770 --> 00:49:16,310 to Es-- if that line has a slope of 1, 752 00:49:16,310 --> 00:49:20,040 then we're just moving up and down with respect to Es. 753 00:49:20,040 --> 00:49:22,300 So what we do is we scoot up the line 754 00:49:22,300 --> 00:49:25,700 to get to the point that's on the right strain rate. 755 00:49:25,700 --> 00:49:28,720 So if this was a strain rate of 100, or around 200, 756 00:49:28,720 --> 00:49:31,590 we want to be at point B. And then from point B, 757 00:49:31,590 --> 00:49:35,380 we can read off what's the value of W over Es, 758 00:49:35,380 --> 00:49:36,960 and sigma p over Es. 759 00:49:36,960 --> 00:49:39,650 And from that, we can back out what the solid modulus we want 760 00:49:39,650 --> 00:49:40,350 is. 761 00:49:40,350 --> 00:49:43,560 So these are the values that we read off the chart. 762 00:49:43,560 --> 00:49:46,930 This gives us an Es of 28 mega Pascals. 763 00:49:46,930 --> 00:49:50,240 And again, you can go to this more detailed diagram here, 764 00:49:50,240 --> 00:49:53,790 and if you read off the sigma p over Es, and the W over Es, 765 00:49:53,790 --> 00:49:56,370 the density you want is about 0.1. 766 00:49:56,370 --> 00:49:58,092 So it tells you the modulus of the solid, 767 00:49:58,092 --> 00:49:59,550 and from that you can pick a solid, 768 00:49:59,550 --> 00:50:02,060 and it tells you the density. 769 00:50:02,060 --> 00:50:04,232 Are we good? 770 00:50:04,232 --> 00:50:05,190 OK, so I have one more. 771 00:50:05,190 --> 00:50:08,154 So there's a slightly different way you can do it, too. 772 00:50:08,154 --> 00:50:10,320 So now I want to talk about bicycle helmets-- you're 773 00:50:10,320 --> 00:50:11,400 my bicycle helmet person. 774 00:50:14,040 --> 00:50:15,810 So this is another little case study 775 00:50:15,810 --> 00:50:18,990 that involves a slightly different way to do this. 776 00:50:18,990 --> 00:50:21,410 And this involves a slightly different diagram. 777 00:50:21,410 --> 00:50:24,859 So the idea here is to choose a material for a bicycle helmet. 778 00:50:24,859 --> 00:50:26,900 And as you probably all know, the bicycle helmets 779 00:50:26,900 --> 00:50:29,700 have a hard shell, and they have some sort of foamy liner. 780 00:50:29,700 --> 00:50:32,660 And the foam's usually around 20 millimeters thick. 781 00:50:32,660 --> 00:50:34,244 And you want something that's light, 782 00:50:34,244 --> 00:50:36,410 because you don't want your helmet to be too heavy-- 783 00:50:36,410 --> 00:50:38,035 but you want something that will absorb 784 00:50:38,035 --> 00:50:39,310 the energy from the impact. 785 00:50:39,310 --> 00:50:43,760 So I've set this up here-- so we assume the mass of the head 786 00:50:43,760 --> 00:50:45,610 is about 3 kilograms. 787 00:50:45,610 --> 00:50:47,170 And we assume that it can withstand 788 00:50:47,170 --> 00:50:50,120 a deceleration of something like 300g-- 789 00:50:50,120 --> 00:50:53,190 and so then you can get a force mass times the acceleration, 790 00:50:53,190 --> 00:50:54,460 because you have the force. 791 00:50:54,460 --> 00:50:56,460 And I've assumed an area of contact of something 792 00:50:56,460 --> 00:51:01,270 like 0.01 meters squared, so that gives you a peak stress. 793 00:51:01,270 --> 00:51:04,150 So this method here is based on the idea 794 00:51:04,150 --> 00:51:07,590 that you have these material selection charts for foams. 795 00:51:07,590 --> 00:51:09,770 Remember we talked about that earlier. 796 00:51:09,770 --> 00:51:12,660 And this is the compressive stress at 25% strain. 797 00:51:12,660 --> 00:51:14,350 So the idea is that axis there is 798 00:51:14,350 --> 00:51:16,590 meant to represent the plateau stress, 799 00:51:16,590 --> 00:51:20,060 and this axis here represents the densification strain. 800 00:51:20,060 --> 00:51:22,950 And these dashed lines here correspond 801 00:51:22,950 --> 00:51:26,090 to basically a value of W-- and energy 802 00:51:26,090 --> 00:51:28,290 absorbed per unit volume. 803 00:51:28,290 --> 00:51:30,380 So this is an energy absorbed per unit volume 804 00:51:30,380 --> 00:51:35,470 of 0.001 megajoules per cubic meter, 0.01, and so on. 805 00:51:35,470 --> 00:51:39,846 So if you know the peak stress that you can tolerate, 806 00:51:39,846 --> 00:51:41,470 for the numbers I gave you it works out 807 00:51:41,470 --> 00:51:45,220 to be 0.9 mega Pascals-- so here it's just a little less than 1. 808 00:51:45,220 --> 00:51:48,240 So that's the peak stress that you can tolerate there. 809 00:51:48,240 --> 00:51:51,800 And you can see that the material that's 810 00:51:51,800 --> 00:51:55,040 going to absorb the most energy-- so you're absorbing 811 00:51:55,040 --> 00:51:59,040 more energy as you move over this way on the curve 812 00:51:59,040 --> 00:52:01,820 on the plot-- so the material that's going to do the best 813 00:52:01,820 --> 00:52:05,480 is something like an expanded polystyrene that's 5% dense. 814 00:52:05,480 --> 00:52:07,440 So I've highlighted that in red-- expanded 815 00:52:07,440 --> 00:52:10,030 polystyrene that's 5% dense. 816 00:52:10,030 --> 00:52:13,060 And then this is the densification strain here. 817 00:52:13,060 --> 00:52:15,510 And you know that the lines of the energy absorption 818 00:52:15,510 --> 00:52:18,580 are just the stress times the strain. 819 00:52:18,580 --> 00:52:20,580 So you can basically just read off from here 820 00:52:20,580 --> 00:52:22,940 that expanded polystyrene that was 5% dense 821 00:52:22,940 --> 00:52:26,680 would be a good choice for a bicycle helmet foam. 822 00:52:26,680 --> 00:52:30,570 Would you like to add anything about bicycle helmet foams? 823 00:52:30,570 --> 00:52:33,850 I think that is exactly what they use, yes. 824 00:52:33,850 --> 00:52:36,180 So this is just another way to do this kind of thing. 825 00:52:36,180 --> 00:52:38,640 And I did one more little calculation here-- 826 00:52:38,640 --> 00:52:42,340 if you know the thickness of the foam is, say, 20 millimeters, 827 00:52:42,340 --> 00:52:45,110 and we've estimated the area of the contact, 828 00:52:45,110 --> 00:52:47,980 you can figure out what the energy absorbed is 829 00:52:47,980 --> 00:52:49,970 per unit volume, and from that you can back out 830 00:52:49,970 --> 00:52:53,020 the energy in terms of joules, and from that you can back out 831 00:52:53,020 --> 00:52:56,170 the velocity that's the maximum speed that one 832 00:52:56,170 --> 00:52:59,490 would want to get dinged at on your bicycle. 833 00:52:59,490 --> 00:53:02,540 And the maximum speed works out about 22 miles an hour. 834 00:53:02,540 --> 00:53:06,190 So that's just another example. 835 00:53:06,190 --> 00:53:07,750 Are we good? 836 00:53:07,750 --> 00:53:11,592 OK-- yeah, exactly, your head would 837 00:53:11,592 --> 00:53:13,300 be hitting the ground at 22 miles an hour 838 00:53:13,300 --> 00:53:14,730 which, would be ouchy. 839 00:53:14,730 --> 00:53:17,310 Which is why you want to wear your helmet, 840 00:53:17,310 --> 00:53:20,126 because your skull will not be happy if that happens. 841 00:53:20,126 --> 00:53:21,500 And your brain will not be happy. 842 00:53:21,500 --> 00:53:23,110 And you will not be happy. 843 00:53:23,110 --> 00:53:26,780 And your mom and dad will be really, really, really unhappy. 844 00:53:26,780 --> 00:53:29,470 So you don't want that to happen. 845 00:53:29,470 --> 00:53:31,540 so I have a few minutes left-- and I 846 00:53:31,540 --> 00:53:33,464 know I've done this for the people in 3032, 847 00:53:33,464 --> 00:53:35,630 but I was going to buy woodpecker talk, because it's 848 00:53:35,630 --> 00:53:37,420 about energy absorption. 849 00:53:37,420 --> 00:53:39,920 So if you don't want to watch it, if you've already seen it, 850 00:53:39,920 --> 00:53:40,572 you can go. 851 00:53:40,572 --> 00:53:42,780 But there are some people-- you guys haven't seen it, 852 00:53:42,780 --> 00:53:43,590 and you haven't seen it. 853 00:53:43,590 --> 00:53:45,215 There's a few people that haven't seen. 854 00:53:45,215 --> 00:53:47,222 And it's cute, involves birds. 855 00:53:47,222 --> 00:53:48,680 And it involves energy absorption-- 856 00:53:48,680 --> 00:53:50,576 so I thought I would do this woodpecker talk. 857 00:53:56,830 --> 00:53:58,510 So Barry, this is all just slides. 858 00:53:58,510 --> 00:54:01,310 I don't know if you want to do the lights differently. 859 00:54:01,310 --> 00:54:02,590 I'm not going to write anything on the board, 860 00:54:02,590 --> 00:54:03,440 I'm just going to talk. 861 00:54:03,440 --> 00:54:05,172 BARRY: Well, if it will help them see the slides better then 862 00:54:05,172 --> 00:54:05,550 certainly. 863 00:54:05,550 --> 00:54:07,050 LORNA GIBSON: Yeah, I think maybe we 864 00:54:07,050 --> 00:54:09,021 could turn the lights down a little, please. 865 00:54:16,210 --> 00:54:18,240 BARRY: Let's try this one. 866 00:54:18,240 --> 00:54:19,490 LORNA GIBSON: Oh, there we go. 867 00:54:19,490 --> 00:54:20,060 That's good. 868 00:54:20,060 --> 00:54:22,920 Yeah, now I don't feel like I'm looking in the spotlight 869 00:54:22,920 --> 00:54:23,420 so much. 870 00:54:23,420 --> 00:54:24,510 That's good. 871 00:54:24,510 --> 00:54:28,380 OK, so you guys know that I like to watch birds. 872 00:54:28,380 --> 00:54:31,150 And you know that I work on foams. 873 00:54:31,150 --> 00:54:34,040 And if you look at bird books, sometimes the bird books 874 00:54:34,040 --> 00:54:37,940 say that woodpeckers can withstand the impact 875 00:54:37,940 --> 00:54:40,590 from pecking because they have a special material 876 00:54:40,590 --> 00:54:42,550 between their skulls and their brains. 877 00:54:42,550 --> 00:54:44,550 And I thought, oh, well I study foams, 878 00:54:44,550 --> 00:54:46,850 and I'm interested in woodpeckers-- I should find out 879 00:54:46,850 --> 00:54:48,440 what this special material is. 880 00:54:48,440 --> 00:54:49,980 So I started looking into this. 881 00:54:49,980 --> 00:54:52,180 And it turns out there is no special material. 882 00:54:52,180 --> 00:54:55,160 People have looked at the anatomy of woodpecker brains 883 00:54:55,160 --> 00:54:57,660 and skulls, and there is no special material. 884 00:54:57,660 --> 00:55:00,020 But it turns out there were also a group of neurologists 885 00:55:00,020 --> 00:55:02,740 in the late 1970s who got interested in why woodpeckers 886 00:55:02,740 --> 00:55:05,610 don't get brain injury, and they took high speed video 887 00:55:05,610 --> 00:55:06,710 of a woodpecker pecking. 888 00:55:06,710 --> 00:55:09,110 And it was kind of amazing what they found out. 889 00:55:09,110 --> 00:55:11,230 So it turns out the woodpeckers can withstand 890 00:55:11,230 --> 00:55:14,810 incredibly high decelerations-- much higher than our brains 891 00:55:14,810 --> 00:55:15,684 could withstand. 892 00:55:15,684 --> 00:55:17,350 And so I kind of got interested in this, 893 00:55:17,350 --> 00:55:21,050 and I decided to try to figure out how it works. 894 00:55:21,050 --> 00:55:23,650 So here's an acorn woodpecker. 895 00:55:23,650 --> 00:55:27,590 And let's see-- I got a little video here. 896 00:55:27,590 --> 00:55:30,860 Wait a minute-- there we go. 897 00:55:30,860 --> 00:55:31,420 There we go. 898 00:55:31,420 --> 00:55:32,920 So here's a little acorn woodpecker. 899 00:55:32,920 --> 00:55:34,160 These live in California. 900 00:55:34,160 --> 00:55:35,510 Anybody from California? 901 00:55:35,510 --> 00:55:37,570 Yeah-- have you seen them? 902 00:55:37,570 --> 00:55:39,430 No, OK. 903 00:55:39,430 --> 00:55:41,230 Well you have not been looking carefully. 904 00:55:41,230 --> 00:55:44,810 So here's our little acorn-- and you can see they peck-- oh? 905 00:55:44,810 --> 00:55:46,240 Like around San Francisco. 906 00:55:46,240 --> 00:55:48,586 AUDIENCE: [INAUDIBLE]. 907 00:55:48,586 --> 00:55:50,520 [LAUGHS] 908 00:55:50,520 --> 00:55:52,010 LORNA GIBSON: So they're pecking, 909 00:55:52,010 --> 00:55:54,760 and when they're pecking-- they don't just go bonk. 910 00:55:54,760 --> 00:55:58,190 They do this repeatedly-- they can peck at 10 or 20 times 911 00:55:58,190 --> 00:55:59,300 per second. 912 00:55:59,300 --> 00:56:03,450 So the question is, why don't they get brain injury? 913 00:56:03,450 --> 00:56:05,720 So, first of all, why do they peck? 914 00:56:05,720 --> 00:56:08,520 So as we in that little video, that woodpecker 915 00:56:08,520 --> 00:56:10,860 was foraging-- it was trying to get little things out 916 00:56:10,860 --> 00:56:11,470 of the bark. 917 00:56:11,470 --> 00:56:16,320 And woodpeckers eat insects, and so the bird books 918 00:56:16,320 --> 00:56:18,890 say that they can actually hear insects scurrying around 919 00:56:18,890 --> 00:56:21,300 under the bark, and they'll peck at the bark 920 00:56:21,300 --> 00:56:23,607 and forage to try to get insects. 921 00:56:23,607 --> 00:56:25,940 And there's one other anatomical feature of woodpeckers, 922 00:56:25,940 --> 00:56:28,601 which is kind of amazing-- and you can see it in this picture 923 00:56:28,601 --> 00:56:29,100 here. 924 00:56:29,100 --> 00:56:31,094 So this is the woodpecker tongue, 925 00:56:31,094 --> 00:56:32,760 and the tongue is connected to something 926 00:56:32,760 --> 00:56:34,210 called the hyoid process. 927 00:56:34,210 --> 00:56:37,736 And the hyoid process wraps around their eyeballs. 928 00:56:37,736 --> 00:56:39,110 And then when they peck-- I mean, 929 00:56:39,110 --> 00:56:41,840 the idea is they're making a hole in the tree, 930 00:56:41,840 --> 00:56:43,930 and they've got to get their tongue into the hole 931 00:56:43,930 --> 00:56:44,950 to get the bug. 932 00:56:44,950 --> 00:56:47,610 And the end of their tongue has little barbs on it. 933 00:56:47,610 --> 00:56:50,150 And when they contract this thing here, 934 00:56:50,150 --> 00:56:53,280 their tongue scoots out and gets the little bugs. 935 00:56:53,280 --> 00:56:56,020 So they pick partly to forage, but they also 936 00:56:56,020 --> 00:56:58,220 build something called cavity nests. 937 00:56:58,220 --> 00:57:01,000 So they'll find a tree that's started to rot, 938 00:57:01,000 --> 00:57:03,500 and they'll drill a sort of horizontal hole, 939 00:57:03,500 --> 00:57:05,542 and then they'll drill a cup underneath that, 940 00:57:05,542 --> 00:57:07,250 and they lay the eggs and have their nest 941 00:57:07,250 --> 00:57:08,577 at the bottom of the cup. 942 00:57:08,577 --> 00:57:11,160 And then they also-- especially at this time of year, in fact, 943 00:57:11,160 --> 00:57:13,600 today I heard woodpeckers drumming-- 944 00:57:13,600 --> 00:57:16,890 so it's one of these mating things, one of these courtship 945 00:57:16,890 --> 00:57:17,390 things. 946 00:57:17,390 --> 00:57:21,210 So woodpeckers will peck on a hollow branch or a hollow tree, 947 00:57:21,210 --> 00:57:23,400 just to make a big loud noise to say, 948 00:57:23,400 --> 00:57:28,150 here I am, looking for sex, I'm ready, this is my territory. 949 00:57:28,150 --> 00:57:30,200 And so in the spring-- so this time of year 950 00:57:30,200 --> 00:57:31,780 you hear woodpeckers drumming. 951 00:57:31,780 --> 00:57:35,380 And I think naturally they do this on hollow trees 952 00:57:35,380 --> 00:57:36,880 to try to make a big sound, but they 953 00:57:36,880 --> 00:57:40,380 have adapted to metal downspouts, which 954 00:57:40,380 --> 00:57:43,350 are also very effective for making this loud noise. 955 00:57:43,350 --> 00:57:45,660 And people who've-- I wrote a paper on this-- 956 00:57:45,660 --> 00:57:48,202 people who have read my paper sometimes email me and say, oh, 957 00:57:48,202 --> 00:57:49,951 I heard you know about woodpecker pecking. 958 00:57:49,951 --> 00:57:52,180 How can I get them to stop drumming on my downspout? 959 00:57:52,180 --> 00:57:53,360 Because it's kind of annoying, if you're 960 00:57:53,360 --> 00:57:54,850 the human inside the house. 961 00:57:54,850 --> 00:57:57,470 So anyway, they peck for these reasons. 962 00:57:57,470 --> 00:57:59,990 And then acorn woodpeckers are special-- acorn woodpeckers 963 00:57:59,990 --> 00:58:03,320 are what I think of as the champions of pecking. 964 00:58:03,320 --> 00:58:05,260 And they do one more behavior-- so 965 00:58:05,260 --> 00:58:08,510 here's from David Sibley's beautiful Guide to Birds, 966 00:58:08,510 --> 00:58:10,160 here's the acorn woodpecker. 967 00:58:10,160 --> 00:58:12,850 They store acorns in what's called a granary, 968 00:58:12,850 --> 00:58:18,360 and they look at old tree trunks that are beginning to rot, 969 00:58:18,360 --> 00:58:20,560 and they pick holes in the tree trunk 970 00:58:20,560 --> 00:58:22,530 and they store the acorns in the holes. 971 00:58:22,530 --> 00:58:25,510 So see all those little dark dots on that trunk? 972 00:58:25,510 --> 00:58:29,310 Those are all holes that the acorn woodpecker has pecked. 973 00:58:29,310 --> 00:58:31,430 And they'll do this-- they live in social groups, 974 00:58:31,430 --> 00:58:34,530 so there might be like 10 or 20 of them living together, 975 00:58:34,530 --> 00:58:38,210 and they'll peck like 10,000 holes into their granary. 976 00:58:38,210 --> 00:58:40,960 There will be thousands and thousands of these holes. 977 00:58:40,960 --> 00:58:42,550 And here we have the acorn woodpecker 978 00:58:42,550 --> 00:58:46,390 with the acorn in its beak, and you can see some of these holes 979 00:58:46,390 --> 00:58:48,120 have acorns, and some of them are empty. 980 00:58:48,120 --> 00:58:51,350 So here is the acorn woodpecker in action. 981 00:58:51,350 --> 00:58:53,940 And here's the little video again-- I won't play the video. 982 00:58:53,940 --> 00:58:56,140 So I often give this talk for non-engineers, 983 00:58:56,140 --> 00:58:58,290 so I'm going to explain some things-- there's 984 00:58:58,290 --> 00:58:59,370 going to be some writing on the slides 985 00:58:59,370 --> 00:59:00,660 that you guys already know. 986 00:59:00,660 --> 00:59:03,180 So the impact force depends on the deceleration-- 987 00:59:03,180 --> 00:59:06,969 how quickly the brain stops when the beak hits the tree. 988 00:59:06,969 --> 00:59:09,260 And I should mention, these videos are from the Cornell 989 00:59:09,260 --> 00:59:13,420 Lab of Ornithology-- they have an amazing collection of bird 990 00:59:13,420 --> 00:59:17,890 audio, like bird calls, bird songs, and bird photographs 991 00:59:17,890 --> 00:59:18,600 and videos. 992 00:59:18,600 --> 00:59:22,730 It's incredible, the collection that they've got. 993 00:59:22,730 --> 00:59:24,320 And then I explain what acceleration 994 00:59:24,320 --> 00:59:26,650 is-- so I'm going to put acceleration 995 00:59:26,650 --> 00:59:27,740 in terms of gravity. 996 00:59:27,740 --> 00:59:29,720 And when the beak hits the tree, there's 997 00:59:29,720 --> 00:59:32,250 going to be a deceleration on impact. 998 00:59:32,250 --> 00:59:34,790 And just as a comparison, human brain injury 999 00:59:34,790 --> 00:59:37,500 occurs roughly at about 100g. 1000 00:59:37,500 --> 00:59:40,200 And so the question is, how much deceleration 1001 00:59:40,200 --> 00:59:42,350 can the woodpecker brain take? 1002 00:59:42,350 --> 00:59:45,820 And that's where the neurologists in the Bay Area 1003 00:59:45,820 --> 00:59:47,230 come into the picture. 1004 00:59:47,230 --> 00:59:49,910 They found out that there was a park 1005 00:59:49,910 --> 00:59:53,110 ranger-- I think maybe at Point Reyes, just north 1006 00:59:53,110 --> 00:59:54,440 of San Francisco. 1007 00:59:54,440 --> 00:59:56,702 And he had an acorn woodpecker that, I don't, had 1008 00:59:56,702 --> 00:59:57,910 an injured wing or something. 1009 00:59:57,910 --> 01:00:01,810 Anyway, he had this acorn woodpecker that he kept. 1010 01:00:01,810 --> 01:00:05,440 And they were able to use this acorn woodpecker, 1011 01:00:05,440 --> 01:00:08,760 and they took high-speed video of the woodpecker pecking. 1012 01:00:08,760 --> 01:00:11,523 So from the high-speed video, the video that they took 1013 01:00:11,523 --> 01:00:14,260 went at something like 2,000 frames a second. 1014 01:00:14,260 --> 01:00:17,420 So they have a picture of where the head is every 2,000th 1015 01:00:17,420 --> 01:00:18,459 of a second. 1016 01:00:18,459 --> 01:00:20,250 So if you know the position at these times, 1017 01:00:20,250 --> 01:00:23,900 you can get the velocity, and you can get the deceleration. 1018 01:00:23,900 --> 01:00:25,510 So they measured the deceleration, 1019 01:00:25,510 --> 01:00:27,470 and they measured some amazing things. 1020 01:00:27,470 --> 01:00:30,510 So they measured that on impact, the woodpecker's bill 1021 01:00:30,510 --> 01:00:33,090 was going something like 15 miles an hour. 1022 01:00:33,090 --> 01:00:35,570 And the decelerations were up to 1,500g-- 1023 01:00:35,570 --> 01:00:39,450 so many times more than what we can withstand. 1024 01:00:39,450 --> 01:00:41,240 And they also measured the stopping time-- 1025 01:00:41,240 --> 01:00:45,190 and they thought it was between about 1/500th to 1/1,000th 1026 01:00:45,190 --> 01:00:45,970 of a second. 1027 01:00:45,970 --> 01:00:48,889 And that's going to be important later on. 1028 01:00:48,889 --> 01:00:50,680 So one of the interesting things about this 1029 01:00:50,680 --> 01:00:52,810 was how they got this whole thing set up. 1030 01:00:52,810 --> 01:00:55,150 So I don't know how many of you do UROPs-- but you know, 1031 01:00:55,150 --> 01:00:56,960 part of the thing in doing UROPs, and doing experiments 1032 01:00:56,960 --> 01:00:58,950 in the lab is just how do you do the experiments? 1033 01:00:58,950 --> 01:01:01,241 So you know, the park rangers got the acorn woodpecker, 1034 01:01:01,241 --> 01:01:02,332 that's all very good. 1035 01:01:02,332 --> 01:01:03,790 But they have to get the woodpecker 1036 01:01:03,790 --> 01:01:05,340 to peck in front of a camera, and they 1037 01:01:05,340 --> 01:01:06,714 have to get the camera to turn on 1038 01:01:06,714 --> 01:01:09,890 as it's pecking-- so there's some experimental challenges. 1039 01:01:09,890 --> 01:01:11,710 So the important thing, the critical thing, 1040 01:01:11,710 --> 01:01:12,960 is the date of the paper. 1041 01:01:12,960 --> 01:01:15,780 This was written in 1979, which meant they probably 1042 01:01:15,780 --> 01:01:17,770 did the experiments in 1978. 1043 01:01:17,770 --> 01:01:19,960 And I was a graduate student in 1978. 1044 01:01:19,960 --> 01:01:24,010 And I can report there were no Apple computers in 1978-- 1045 01:01:24,010 --> 01:01:25,360 there were no laptops. 1046 01:01:25,360 --> 01:01:28,280 You couldn't just kind of do your little PowerPoint slides. 1047 01:01:28,280 --> 01:01:31,530 And most offices had something called an IBM Selectric 1048 01:01:31,530 --> 01:01:34,240 typewriter-- I don't know if you've ever seen the old IBM 1049 01:01:34,240 --> 01:01:35,089 typewriters. 1050 01:01:35,089 --> 01:01:37,380 But the typewriters, when you typed on the typewriters, 1051 01:01:37,380 --> 01:01:39,730 they made these noises, and it sounded kind of 1052 01:01:39,730 --> 01:01:41,180 like a woodpecker pecking. 1053 01:01:41,180 --> 01:01:44,410 And the ranger had one of these typewriters in his office, 1054 01:01:44,410 --> 01:01:46,786 and he had discovered that if he typed on the typewriter, 1055 01:01:46,786 --> 01:01:49,076 the woodpecker thought, oh, there's another woodpecker. 1056 01:01:49,076 --> 01:01:49,990 I'll start pecking. 1057 01:01:49,990 --> 01:01:51,700 And so they used the typewriter as a way 1058 01:01:51,700 --> 01:01:53,310 to get the woodpeckers to peck. 1059 01:01:53,310 --> 01:01:54,810 And I think they had some old stump, 1060 01:01:54,810 --> 01:01:56,620 and I don't know if they put nuts or peanut butter 1061 01:01:56,620 --> 01:01:58,390 or something into the stump to get the woodpecker 1062 01:01:58,390 --> 01:01:59,350 to peck at it-- because they needed 1063 01:01:59,350 --> 01:02:01,724 to peck at a particular spot, so they have the camera all 1064 01:02:01,724 --> 01:02:02,310 set up. 1065 01:02:02,310 --> 01:02:04,530 So anyway, they had this whole arrangement 1066 01:02:04,530 --> 01:02:10,230 to do this high-speed video of the woodpecker pecking. 1067 01:02:10,230 --> 01:02:12,190 OK, so it goes that up to 1,500g, 1068 01:02:12,190 --> 01:02:13,380 which is kind of amazing. 1069 01:02:13,380 --> 01:02:15,900 And then, remember also, they do this repeatedly-- 1070 01:02:15,900 --> 01:02:19,185 they do it at like 10 or 20 times a second. 1071 01:02:19,185 --> 01:02:20,560 Then this is just explaining what 1072 01:02:20,560 --> 01:02:22,560 stress is-- but you already know what stress is, 1073 01:02:22,560 --> 01:02:24,580 so I'm going to skip over that. 1074 01:02:24,580 --> 01:02:26,520 And so the way you can think about this 1075 01:02:26,520 --> 01:02:29,420 is to think about it in terms of a scaling argument. 1076 01:02:29,420 --> 01:02:31,610 So imagine there's the brain and there's the skull, 1077 01:02:31,610 --> 01:02:34,450 and when the head hits the tree, the brain's going 1078 01:02:34,450 --> 01:02:37,010 to accelerate, and the brain and the skull 1079 01:02:37,010 --> 01:02:38,790 are both going to decelerate. 1080 01:02:38,790 --> 01:02:43,470 And you can think of the stress as the force over the area. 1081 01:02:43,470 --> 01:02:46,680 So the force is the mass times the deceleration over the area. 1082 01:02:46,680 --> 01:02:50,470 So that value for the woodpecker, you can say, 1083 01:02:50,470 --> 01:02:54,460 is roughly equal to the same values, but for the human. 1084 01:02:54,460 --> 01:02:58,290 So what that argument relies on is the idea 1085 01:02:58,290 --> 01:03:01,300 that the stress to cause damage in the woodpecker brain 1086 01:03:01,300 --> 01:03:03,910 is similar to the stress to cause damage 1087 01:03:03,910 --> 01:03:05,320 in the human brain. 1088 01:03:05,320 --> 01:03:08,310 And that's not totally unreasonable. 1089 01:03:08,310 --> 01:03:10,201 So if you look at bone, for example, 1090 01:03:10,201 --> 01:03:12,450 like when you measure the strength of the whale bones, 1091 01:03:12,450 --> 01:03:14,100 it's not going to be that different from what you 1092 01:03:14,100 --> 01:03:15,630 would measure from human bones. 1093 01:03:15,630 --> 01:03:18,850 So when you look at a particular type of tissue, 1094 01:03:18,850 --> 01:03:21,692 and you look at the strength of it in different species, 1095 01:03:21,692 --> 01:03:23,900 the properties aren't that different from one species 1096 01:03:23,900 --> 01:03:24,810 to another. 1097 01:03:24,810 --> 01:03:27,470 So let's say the brain tissue gets 1098 01:03:27,470 --> 01:03:31,010 damaged at the same stress in the two species. 1099 01:03:31,010 --> 01:03:33,250 So we can write this sort of equation down. 1100 01:03:33,250 --> 01:03:39,310 And the mass is going to depend on the density of the brain 1101 01:03:39,310 --> 01:03:41,750 tissue times the volume-- and the volume 1102 01:03:41,750 --> 01:03:43,380 goes as the radius cubed. 1103 01:03:43,380 --> 01:03:46,035 And the density is going to be the same for the woodpecker, 1104 01:03:46,035 --> 01:03:48,290 or for the human-- so assume the brain tissue has 1105 01:03:48,290 --> 01:03:50,380 the same kind of basic stuff. 1106 01:03:50,380 --> 01:03:53,760 So the mass goes as the radius cubed, and the area of contact 1107 01:03:53,760 --> 01:03:55,880 is going to go as the radius squared. 1108 01:03:55,880 --> 01:03:57,790 And so there's a radius term. 1109 01:03:57,790 --> 01:03:59,870 So you can say the radius times the deceleration 1110 01:03:59,870 --> 01:04:02,290 in the woodpecker should be equal to the radius 1111 01:04:02,290 --> 01:04:04,470 times the deceleration of the human. 1112 01:04:04,470 --> 01:04:06,000 And obviously, the woodpecker radius 1113 01:04:06,000 --> 01:04:09,104 is going to be a lot smaller, so the woodpecker deceleration 1114 01:04:09,104 --> 01:04:10,270 is going to be a lot bigger. 1115 01:04:10,270 --> 01:04:13,930 So part of the thing is the brain is just a lot smaller. 1116 01:04:13,930 --> 01:04:16,510 Then there's another factor that comes into it-- 1117 01:04:16,510 --> 01:04:20,390 these are photographs of an acorn woodpecker 1118 01:04:20,390 --> 01:04:22,740 skull and a human skull that I got 1119 01:04:22,740 --> 01:04:25,790 from the Museum of Comparative Zoology at Harvard. 1120 01:04:25,790 --> 01:04:27,490 So this is looking down on the top, 1121 01:04:27,490 --> 01:04:29,866 and this is an elevation view. 1122 01:04:29,866 --> 01:04:32,490 And if you think of the brain as roughly a hemisphere-- I mean, 1123 01:04:32,490 --> 01:04:33,850 obviously it's not a perfect hemisphere, 1124 01:04:33,850 --> 01:04:35,558 but let's say it's roughly a hemisphere-- 1125 01:04:35,558 --> 01:04:37,750 the orientation of the brain in the skull 1126 01:04:37,750 --> 01:04:40,309 is slightly different in the birds and in the human. 1127 01:04:40,309 --> 01:04:42,100 So if you think of it as being this way on, 1128 01:04:42,100 --> 01:04:45,540 and in the woodpecker it's turned roughly this way on, 1129 01:04:45,540 --> 01:04:48,480 and the contact area-- think of this as the contact area. 1130 01:04:48,480 --> 01:04:51,590 The projected area would be a full circle, and in the human, 1131 01:04:51,590 --> 01:04:53,240 the brain is more this way on. 1132 01:04:53,240 --> 01:04:56,800 And then the projected contact area is a semicircle. 1133 01:04:56,800 --> 01:04:58,540 So there's a factor of 2 difference, 1134 01:04:58,540 --> 01:05:01,910 just because of the orientation of the brain. 1135 01:05:01,910 --> 01:05:04,970 And so I've put the factor of 2 that accounts for that. 1136 01:05:04,970 --> 01:05:06,470 So then I could say the deceleration 1137 01:05:06,470 --> 01:05:08,800 that the woodpecker can take is twice 1138 01:05:08,800 --> 01:05:11,940 the ratio of the radii of the human and the woodpecker brain, 1139 01:05:11,940 --> 01:05:13,730 times the deceleration the human can take. 1140 01:05:13,730 --> 01:05:16,080 And this was around 100g, remember. 1141 01:05:16,080 --> 01:05:18,440 So then I wanted to know what the ratio of the sizes 1142 01:05:18,440 --> 01:05:19,910 was, and I thought, oh geez-- I'm 1143 01:05:19,910 --> 01:05:22,190 going to have to mess around with skulls, 1144 01:05:22,190 --> 01:05:23,940 and try to make some sort of measurements, 1145 01:05:23,940 --> 01:05:25,320 and this is going to be a drag. 1146 01:05:25,320 --> 01:05:27,630 And then I found this paper-- I couldn't believe it-- 1147 01:05:27,630 --> 01:05:29,830 I found this paper called "Brain Size in Birds." 1148 01:05:29,830 --> 01:05:31,700 And this guy had table after table 1149 01:05:31,700 --> 01:05:34,910 after table of the mass of the brain in different birds-- 1150 01:05:34,910 --> 01:05:37,720 and he had the acorn woodpecker, lucky for me. 1151 01:05:37,720 --> 01:05:40,804 So if you just assume that the brain is roughly a hemisphere, 1152 01:05:40,804 --> 01:05:42,720 if you have the mass, you can work out roughly 1153 01:05:42,720 --> 01:05:44,030 what the radius is. 1154 01:05:44,030 --> 01:05:45,880 So it turns out there's a factor of 8 1155 01:05:45,880 --> 01:05:48,600 difference between the radii. 1156 01:05:48,600 --> 01:05:51,880 And so the human brain is about eight times the size 1157 01:05:51,880 --> 01:05:53,030 of the woodpecker. 1158 01:05:53,030 --> 01:05:55,292 And then if you take into account this factor of 2, 1159 01:05:55,292 --> 01:05:56,750 that means the woodpecker should be 1160 01:05:56,750 --> 01:06:01,655 able to tolerate a deceleration of 16 times what the human can. 1161 01:06:01,655 --> 01:06:03,030 So remember, I said the human can 1162 01:06:03,030 --> 01:06:06,490 take about 100-- so this would get the woodpecker up to 1,600. 1163 01:06:06,490 --> 01:06:07,960 But they measured 1,500. 1164 01:06:07,960 --> 01:06:10,280 And I'm a civil engineer, originally, 1165 01:06:10,280 --> 01:06:12,430 I like big factors of safety-- that's a little too 1166 01:06:12,430 --> 01:06:14,630 close for comfort for me. 1167 01:06:14,630 --> 01:06:18,360 And so it turns out there's one more factor that matters. 1168 01:06:18,360 --> 01:06:21,690 People have studied human brain injury pretty extensively, 1169 01:06:21,690 --> 01:06:23,350 and one of the things they've looked at 1170 01:06:23,350 --> 01:06:27,500 is how much acceleration you can tolerate without injury, 1171 01:06:27,500 --> 01:06:29,730 relative to the duration of the impact. 1172 01:06:29,730 --> 01:06:33,337 So this is from a car crash conference-- so here's 1173 01:06:33,337 --> 01:06:34,920 the tolerable acceleration, and here's 1174 01:06:34,920 --> 01:06:36,560 the duration of the impact. 1175 01:06:36,560 --> 01:06:38,480 And typically, for human head impacts, 1176 01:06:38,480 --> 01:06:41,320 the deceleration occurs over a few milliseconds-- 1177 01:06:41,320 --> 01:06:43,950 like over 3 to 10 milliseconds. 1178 01:06:43,950 --> 01:06:46,810 So if this is the duration of the typical head 1179 01:06:46,810 --> 01:06:49,960 impact for a human, here's the range of the tolerable 1180 01:06:49,960 --> 01:06:53,080 accelerations between about 80g and 160g-- so you know, 1181 01:06:53,080 --> 01:06:54,490 I said around 100. 1182 01:06:54,490 --> 01:06:57,650 So we can take this curve, and now we have this factor of 16, 1183 01:06:57,650 --> 01:06:59,760 and we can just scale it up by our factor of 16 1184 01:06:59,760 --> 01:07:01,070 for the woodpecker. 1185 01:07:01,070 --> 01:07:04,660 So if I scale it up by the factor of 16, we're there. 1186 01:07:04,660 --> 01:07:08,264 But the duration of the impacts was more around 1/2 1187 01:07:08,264 --> 01:07:09,930 a millisecond, to a millisecond, so I've 1188 01:07:09,930 --> 01:07:11,730 extrapolated this a little bit. 1189 01:07:11,730 --> 01:07:14,610 And the duration of them is up in here. 1190 01:07:14,610 --> 01:07:16,190 So this is saying the woodpecker can 1191 01:07:16,190 --> 01:07:19,550 take these sorts of decelerations here, 1192 01:07:19,550 --> 01:07:22,180 and that adds on another factor of 4. 1193 01:07:22,180 --> 01:07:25,130 And these were the measured decelerations-- 1194 01:07:25,130 --> 01:07:27,320 1,500 was about the biggest, and I think it 1195 01:07:27,320 --> 01:07:30,510 went to about a few hundred g. 1196 01:07:30,510 --> 01:07:31,935 So there's really three factors-- 1197 01:07:31,935 --> 01:07:33,560 one is the small brain size, so there's 1198 01:07:33,560 --> 01:07:35,470 this sort of scaling factor. 1199 01:07:35,470 --> 01:07:37,140 One is the orientation of the brain, 1200 01:07:37,140 --> 01:07:38,440 that was another factor of 2. 1201 01:07:38,440 --> 01:07:40,148 And then there's this duration of impact, 1202 01:07:40,148 --> 01:07:41,650 which is a factor of 4. 1203 01:07:41,650 --> 01:07:44,377 And so that's how you can get this huge decelerations 1204 01:07:44,377 --> 01:07:46,210 that they've measured in the woodpecker when 1205 01:07:46,210 --> 01:07:48,250 they're pecking. 1206 01:07:48,250 --> 01:07:51,320 So now I have just a couple more slides. 1207 01:07:51,320 --> 01:07:54,640 So woodpeckers have various adaptations to pecking, too. 1208 01:07:54,640 --> 01:07:56,910 So one of the things is they have amazingly stiff tail 1209 01:07:56,910 --> 01:07:58,760 feathers-- you see the tails here? 1210 01:07:58,760 --> 01:08:01,176 You can't quite see it because this didn't reproduce quite 1211 01:08:01,176 --> 01:08:03,750 properly, but the woodpecker is perched on a tree here, 1212 01:08:03,750 --> 01:08:06,197 and the tail is pressed up against the tree. 1213 01:08:06,197 --> 01:08:08,030 And if you think about pecking, like imagine 1214 01:08:08,030 --> 01:08:10,071 if its tail was not pressed up against the tree-- 1215 01:08:10,071 --> 01:08:12,080 it would be kind of grabbing on with its feet, 1216 01:08:12,080 --> 01:08:14,666 and it would be trying to peck, and it would be hard to push. 1217 01:08:14,666 --> 01:08:16,540 You know, you need something to push against. 1218 01:08:16,540 --> 01:08:19,164 And so it's got these stiff tail feathers, which make it easier 1219 01:08:19,164 --> 01:08:22,149 to push against the tree. 1220 01:08:22,149 --> 01:08:24,750 And so here's the stiff tail feathers here. 1221 01:08:24,750 --> 01:08:26,840 It's also got kind of unusual feet 1222 01:08:26,840 --> 01:08:30,011 for birds-- it's got two toes forward and two toes back. 1223 01:08:30,011 --> 01:08:31,760 And again, if it's grabbing with its feet, 1224 01:08:31,760 --> 01:08:35,260 that helps it get some purchase to push against. 1225 01:08:35,260 --> 01:08:38,939 That's called zygodactyl in the bird world. 1226 01:08:38,939 --> 01:08:40,934 So it's got these adaptations, the pecking. 1227 01:08:40,934 --> 01:08:42,600 And then finally, I just like this slide 1228 01:08:42,600 --> 01:08:44,080 here from The New Yorker, because it's 1229 01:08:44,080 --> 01:08:45,760 a woodpecker pecking out a woodpecker, 1230 01:08:45,760 --> 01:08:47,540 so it seemed kind of cute. 1231 01:08:47,540 --> 01:08:50,279 And several people helped me with this project. 1232 01:08:50,279 --> 01:08:52,740 Trey Crisco studies head injury at Brown. 1233 01:08:52,740 --> 01:08:57,520 He actually does work for the NFL on football brain injuries, 1234 01:08:57,520 --> 01:08:58,790 and looks at football helmets. 1235 01:08:58,790 --> 01:09:00,410 Sharon Swartz is a friend of mine at Brown, 1236 01:09:00,410 --> 01:09:01,229 who's a biologist. 1237 01:09:01,229 --> 01:09:02,310 She studies bat flight. 1238 01:09:02,310 --> 01:09:04,720 And she just thought this was kind of a cool project. 1239 01:09:04,720 --> 01:09:09,380 So, in fact, I was walking the dog last week, a few days ago, 1240 01:09:09,380 --> 01:09:11,899 and I saw bats flying around overhead at night. 1241 01:09:11,899 --> 01:09:14,069 And it was so great to see the little bats. 1242 01:09:14,069 --> 01:09:15,979 So I had to immediately email Sharon, 1243 01:09:15,979 --> 01:09:18,240 and say, bats-- there's bats in my neighborhood. 1244 01:09:18,240 --> 01:09:21,470 Andy Biewener runs the Concord Field Station, 1245 01:09:21,470 --> 01:09:23,970 and studies animal locomotion, and I talked to him about it. 1246 01:09:23,970 --> 01:09:26,270 Jeremy Trimble was the one who gave me the skull pictures, 1247 01:09:26,270 --> 01:09:27,770 and Matt Dawson was a student helped 1248 01:09:27,770 --> 01:09:29,840 me do some of the images. 1249 01:09:29,840 --> 01:09:32,120 So that's my woodpecker talk. 1250 01:09:32,120 --> 01:09:33,890 So that's the end of energy absorption, 1251 01:09:33,890 --> 01:09:36,180 I just thought that was kind of amusing. 1252 01:09:36,180 --> 01:09:39,120 So next time, we'll start talking about sandwich panels. 1253 01:09:39,120 --> 01:09:41,170 So, let's see-- Monday's a holiday. 1254 01:09:41,170 --> 01:09:43,754 I will be in Toronto on Monday, seeing my family. 1255 01:09:43,754 --> 01:09:45,920 In fact, I'm going to see one of my old professors-- 1256 01:09:45,920 --> 01:09:48,211 I'm going to my old fluid mechanics professor on Monday 1257 01:09:48,211 --> 01:09:48,880 and have lunch. 1258 01:09:48,880 --> 01:09:50,689 I'll see my family on the weekend. 1259 01:09:50,689 --> 01:09:53,850 And so we'll meet Wednesday next week, 1260 01:09:53,850 --> 01:09:56,550 and I'll start the bit on sandwich panels. 1261 01:09:56,550 --> 01:09:59,860 So I think there's two lectures on engineering sandwich panels, 1262 01:09:59,860 --> 01:10:03,930 and then there's a lecture on natural sandwich panels-- 1263 01:10:03,930 --> 01:10:06,630 so bird skulls, for example, are natural sandwich panels. 1264 01:10:06,630 --> 01:10:07,890 So I'll talk about that. 1265 01:10:07,890 --> 01:10:09,720 And then I think the last lecture-- 1266 01:10:09,720 --> 01:10:12,080 there's only a handful of lectures left-- the last one I 1267 01:10:12,080 --> 01:10:14,475 think I talk about natural materials, because you know, 1268 01:10:14,475 --> 01:10:15,270 I like that. 1269 01:10:15,270 --> 01:10:17,890 So I just do that for fun.