WEBVTT 00:00.209 --> 00:02.450 The Korean War was the newly 00:02.460 --> 00:05.349 independent Air Force's first war . The 00:05.360 --> 00:07.471 air force became independent from the 00:07.471 --> 00:10.779 army in 1947 . In terms of the labs , 00:10.789 --> 00:13.029 the theme that we have here is the use 00:13.039 --> 00:15.619 of World War I I equipment . But then 00:15.630 --> 00:17.686 also the introduction of some of the 00:17.686 --> 00:19.908 new systems and technology developed at 00:19.908 --> 00:22.074 the end . And shortly after the end of 00:22.074 --> 00:26.040 the war , the R 4360 was 00:26.049 --> 00:28.780 the most powerful radial engine used by 00:28.790 --> 00:30.989 the US Air Force and really represents 00:31.000 --> 00:34.090 the ultimate peak of this technology . 00:34.500 --> 00:36.689 At the same time , the 4360 was being 00:36.700 --> 00:39.569 operated jet engines were coming online 00:39.580 --> 00:41.747 and ultimately superseded this kind of 00:41.747 --> 00:43.524 technology . But what's kind of 00:43.524 --> 00:45.858 interesting here is when you look at it , 00:45.858 --> 00:48.869 it has very close similarities to the 00:48.880 --> 00:51.659 very earliest radial engines that we 00:51.669 --> 00:53.860 looked at . That . Uh Sam Herron's 00:53.869 --> 00:56.459 technology helped enable , we see it in 00:56.470 --> 00:58.869 this engine . So it has aluminum 00:58.880 --> 01:02.500 cooling fins and it has a hollow 01:02.549 --> 01:06.459 sodium cooled valves . Um and 01:06.470 --> 01:08.470 it , it's essentially it's multiple 01:08.470 --> 01:10.510 banks . So in some ways , it's no 01:10.519 --> 01:13.230 different from that early radial engine 01:13.239 --> 01:15.461 that we looked at earlier in the tour . 01:15.461 --> 01:17.517 And kind of interesting too . If you 01:17.517 --> 01:19.517 take a look , you can see there's a 01:19.517 --> 01:21.350 supercharger and you can see the 01:21.350 --> 01:23.406 impeller for that right there at the 01:23.406 --> 01:25.517 front of the engine . And we're going 01:25.517 --> 01:27.683 to see a similar shape in an early jet 01:27.683 --> 01:30.750 engine used by the US Air Force . So as 01:30.760 --> 01:32.989 reciprocating engines kind of fell out 01:33.000 --> 01:35.470 of favor and jet engines came online as 01:35.480 --> 01:37.536 the principal form of propulsion for 01:37.536 --> 01:39.550 military aircraft that created 01:39.559 --> 01:41.889 additional problems , problems of air 01:41.900 --> 01:44.830 dynamics . So when we look at this F 80 01:44.839 --> 01:47.150 which was really the first operational 01:47.160 --> 01:49.830 jet fighter used by the US Air Force , 01:49.839 --> 01:52.559 it kind of looks in like a world war I 01:52.569 --> 01:55.089 I fighter , it has straight wings , 01:55.099 --> 01:57.519 it's metal construction , in fact , 01:57.529 --> 01:59.800 aerodynamically , it's essentially like 01:59.809 --> 02:01.753 some of the standard world war I I 02:01.753 --> 02:05.080 fighters used by the USA A F really 02:05.089 --> 02:07.256 doesn't take advantage of the power of 02:07.256 --> 02:10.259 the jet engine behind me . However , in 02:10.270 --> 02:13.460 the distance is the F 86 Saber and 02:13.470 --> 02:15.637 what's important here is the saber has 02:15.637 --> 02:18.690 swept wings and swept wings , allow the 02:18.699 --> 02:20.990 aircraft to take advantage of the power 02:21.000 --> 02:23.500 of the jet engines . And that's where 02:23.509 --> 02:25.740 aerodynamics really come into play . 02:25.910 --> 02:27.854 And we talk about things like wind 02:27.854 --> 02:31.429 tunnels and engineers and looking at 02:31.440 --> 02:33.384 different shapes that work best at 02:33.384 --> 02:35.600 certain speeds that of work is done 02:35.610 --> 02:37.789 today . And the aerospace systems 02:37.800 --> 02:40.559 directorate of Afr L . But one thing to 02:40.570 --> 02:43.509 point out on this F 80 is its intake 02:43.520 --> 02:47.210 and , and actually intakes and inlets 02:47.220 --> 02:49.389 for jet engines are very , very 02:49.399 --> 02:51.639 important and sometimes very , very 02:51.649 --> 02:54.119 difficult to shape . And it's a problem 02:54.130 --> 02:56.297 that our engineers and scientists deal 02:56.297 --> 02:58.740 with in a Fr L even today . And the 02:58.750 --> 03:01.559 case of the F 80 you'll notice that 03:01.570 --> 03:03.737 it's not just a straight intake , it's 03:03.737 --> 03:06.020 actually offset in the front . And 03:06.029 --> 03:08.140 there's a very good reason for that . 03:08.140 --> 03:10.460 The very earliest prototypes of the F 03:10.470 --> 03:13.399 80 had a problem with the boundary 03:13.410 --> 03:15.410 layer and that's the layer of air . 03:15.410 --> 03:17.410 That's right next to the fuselage . 03:17.410 --> 03:19.632 They needed a way to , to not have that 03:19.632 --> 03:22.190 air go into the intake to the engine . 03:22.570 --> 03:24.679 And the device that you see here 03:24.690 --> 03:27.130 actually is a little bit of a standoff 03:27.139 --> 03:29.306 that prevents that boundary layer from 03:29.306 --> 03:31.339 going into the intake . So as we go 03:31.350 --> 03:33.461 through the tour , we're going to see 03:33.461 --> 03:35.572 some other aircraft where the airflow 03:35.572 --> 03:37.572 into the engine played a really big 03:37.572 --> 03:39.899 role in how the aircraft performed and 03:39.910 --> 03:42.132 sometimes it was a really big challenge 03:42.132 --> 03:43.243 with the aircraft . 03:46.139 --> 03:48.306 Now , this display shows two important 03:48.306 --> 03:50.195 technologies developed by the Air 03:50.195 --> 03:52.779 Force's labs . We have an ejection seat 03:52.949 --> 03:55.171 and the lab started working on those in 03:55.171 --> 03:57.116 the late 19 forties . As we had ah 03:57.116 --> 03:59.338 looked at before by the Korean War , we 03:59.338 --> 04:01.360 have a tactical aircraft , fighter 04:01.369 --> 04:03.480 aircraft equipped with ejection seats 04:03.500 --> 04:05.667 and saving the lives of fighter pilots 04:05.667 --> 04:07.556 when they're in danger with their 04:07.556 --> 04:09.333 aircraft . The other technology 04:09.333 --> 04:11.750 represented here is the G suit . Now , 04:11.759 --> 04:13.703 this represents a fighter pilot in 04:13.703 --> 04:16.609 Korea , but army air forces , fighter 04:16.619 --> 04:19.630 pilots were using G suits by 1944 in 04:19.640 --> 04:22.359 Europe . And our labs partnered with 04:22.369 --> 04:24.359 the Mayo Clinic to develop those G 04:24.369 --> 04:26.730 suits and they also benefited from 04:26.739 --> 04:29.369 Canadian and Australian researchers . 04:30.380 --> 04:32.602 Now , what the G suit does is it allows 04:32.602 --> 04:35.200 pilots to pull higher GS . And what A G 04:35.209 --> 04:39.149 is one G is the amount of gravity on 04:39.160 --> 04:41.559 our bodies when we're just standing and 04:41.570 --> 04:44.559 not in motion with high performance 04:44.570 --> 04:47.059 aircraft . When they say , for instance , 04:47.070 --> 04:49.799 pull out from a dive , it pulls GS . So 04:49.809 --> 04:53.140 for instance , five GS would cause that 04:53.149 --> 04:55.940 pilot to weigh five times as much as 04:55.950 --> 04:58.061 they do when they're just standing on 04:58.061 --> 05:00.117 the ground . And the important thing 05:00.117 --> 05:02.283 here is pulling high G causes blood to 05:02.283 --> 05:04.665 drain from the head to the feet . And 05:04.674 --> 05:07.625 what the G suit does using pneumatics , 05:07.635 --> 05:10.015 it constricts the waist and the legs 05:10.035 --> 05:12.804 and lessens the amount of blood that's 05:12.815 --> 05:15.065 draining to the feet , thereby allowing 05:15.075 --> 05:17.404 the pilot to pull higher and faster 05:17.415 --> 05:18.065 turns .