1 00:00:07,040 --> 00:00:03,409 the frontiers of flight have been 2 00:00:10,450 --> 00:00:09,290 highly experimental designs for the 3 00:00:13,280 --> 00:00:10,460 plains of the world 4 00:00:17,179 --> 00:00:13,290 this plane is the latest of the x-series 5 00:00:19,640 --> 00:00:17,189 an aircraft called the x-29 at first 6 00:00:23,180 --> 00:00:19,650 glance the prime seems ordinary until 7 00:00:29,690 --> 00:00:25,120 bring back 8 00:00:34,500 --> 00:00:32,490 through the use of the x-29 is a test 9 00:00:36,750 --> 00:00:34,510 vehicle engineers will be able to 10 00:00:39,870 --> 00:00:36,760 explore the forward swept wings unique 11 00:00:42,660 --> 00:00:39,880 mixture of speed agility and slow flying 12 00:00:44,400 --> 00:00:42,670 qualities they will also explore the 13 00:00:46,979 --> 00:00:44,410 interaction of the wings with the 14 00:00:50,370 --> 00:00:46,989 forward canards and rear straight flaps 15 00:00:52,190 --> 00:00:50,380 in this design all control surfaces are 16 00:00:55,140 --> 00:00:52,200 linked together by computer 17 00:00:59,610 --> 00:00:55,150 Walter sepak NASA's program manager for 18 00:01:04,700 --> 00:00:59,620 the x-29 all three of these surfaces are 19 00:01:07,860 --> 00:01:04,710 tied into a digital computer and their 20 00:01:10,530 --> 00:01:07,870 deflection or movement during flight is 21 00:01:13,140 --> 00:01:10,540 optimized by the flight control 22 00:01:15,600 --> 00:01:13,150 computers when the pilot makes a stick 23 00:01:18,300 --> 00:01:15,610 input to the airplane these three 24 00:01:20,460 --> 00:01:18,310 surfaces all right react simultaneously 25 00:01:23,490 --> 00:01:20,470 to give the optimal response of the 26 00:01:26,100 --> 00:01:23,500 airplane to minimize drag and maximize 27 00:01:28,230 --> 00:01:26,110 performance the forward swept wing 28 00:01:30,510 --> 00:01:28,240 concept was first explored during World 29 00:01:33,090 --> 00:01:30,520 War two when the Germans built a test 30 00:01:36,120 --> 00:01:33,100 bomber with 15 degree forward swept 31 00:01:38,280 --> 00:01:36,130 wings the bomber had a limitation which 32 00:01:41,340 --> 00:01:38,290 is inherent to all forward swept wings 33 00:01:44,130 --> 00:01:41,350 it is called structural divergence and 34 00:01:46,290 --> 00:01:44,140 is illustrated here as soon as higher 35 00:01:47,580 --> 00:01:46,300 speeds are realized the wingtips 36 00:01:50,190 --> 00:01:47,590 experience tremendous 37 00:01:53,610 --> 00:01:50,200 twisting loads which flex the wings and 38 00:01:56,490 --> 00:01:53,620 can literally tear them off the x-29 39 00:01:58,950 --> 00:01:56,500 swing is criss-crossed with 750 40 00:02:02,790 --> 00:01:58,960 composite tapes of such material as 41 00:02:04,920 --> 00:02:02,800 carbon Kevlar and glass the materials 42 00:02:07,260 --> 00:02:04,930 are woven in a way to counteract the 43 00:02:13,870 --> 00:02:07,270 twisting forces encountered by the wing 44 00:02:19,350 --> 00:02:15,520 is to prove the benefits of the 45 00:02:22,410 --> 00:02:19,360 forward-swept wing to confirm the x-29 46 00:02:24,510 --> 00:02:22,420 and when these goals are accomplished to 47 00:02:27,840 --> 00:02:24,520 make sure the results are transferred to 48 00:02:29,970 --> 00:02:27,850 government and industry what we learned 49 00:02:32,250 --> 00:02:29,980 this program will help build the next 50 00:02:33,320 --> 00:02:32,260 generation of fighter and commercial