1 00:00:17,990 --> 00:00:15,990 this f-106 was designed in the mid-1950s 2 00:00:19,910 --> 00:00:18,000 for supersonic flight 3 00:00:22,150 --> 00:00:19,920 nasa's langley research center 4 00:00:24,150 --> 00:00:22,160 originally used the aircraft to study 5 00:00:25,590 --> 00:00:24,160 lightning by flying it directly into 6 00:00:27,750 --> 00:00:25,600 thunderstorms 7 00:00:30,230 --> 00:00:27,760 engineers are now using the plane for 8 00:00:32,709 --> 00:00:30,240 its highly swept wing to explore a 9 00:00:35,910 --> 00:00:32,719 design that incorporates a leading edge 10 00:00:38,630 --> 00:00:35,920 flap an 18-inch wide panel that runs the 11 00:00:41,430 --> 00:00:38,640 length of the wing and points downward 12 00:00:43,510 --> 00:00:41,440 wind tunnel tests with f-106 models 13 00:00:45,990 --> 00:00:43,520 indicate that installing the flap can 14 00:00:47,830 --> 00:00:46,000 increase the plane's performance by more 15 00:00:50,069 --> 00:00:47,840 than 20 percent 16 00:00:52,389 --> 00:00:50,079 265 feet 17 00:00:55,110 --> 00:00:52,399 when air passes over the wings of a 18 00:00:57,270 --> 00:00:55,120 plane small tornado-like currents called 19 00:00:59,270 --> 00:00:57,280 vortices are generated 20 00:01:02,709 --> 00:00:59,280 again look at the wingtip of the space 21 00:01:06,870 --> 00:01:04,229 touchdown 22 00:01:08,950 --> 00:01:06,880 vortices normally form along the entire 23 00:01:11,030 --> 00:01:08,960 wing and are important to aircraft 24 00:01:13,510 --> 00:01:11,040 because they generate lift 25 00:01:17,830 --> 00:01:13,520 looking at a cross-section of the f-106 26 00:01:23,670 --> 00:01:21,109 by adding a vortex flap air is channeled 27 00:01:26,149 --> 00:01:23,680 both upward and forward 28 00:01:28,390 --> 00:01:26,159 according to program manager ron smith 29 00:01:31,510 --> 00:01:28,400 no wings have ever been designed to make 30 00:01:33,910 --> 00:01:31,520 use of this vortex but we're controlling 31 00:01:35,670 --> 00:01:33,920 that vortex that tornado by putting it 32 00:01:39,670 --> 00:01:35,680 on the leading edge where we form a 33 00:01:41,990 --> 00:01:39,680 suction which pulls the airplane along 34 00:01:45,350 --> 00:01:42,000 phil brown is chief test pilot for the 35 00:01:47,749 --> 00:01:45,360 f-106 program he finds the plane much 36 00:01:48,950 --> 00:01:47,759 more responsive with the flap when doing 37 00:01:51,510 --> 00:01:48,960 the movements 38 00:01:53,350 --> 00:01:51,520 this wing design may someday translate 39 00:01:55,590 --> 00:01:53,360 into better handling qualities for 40 00:01:58,230 --> 00:01:55,600 fighter aircraft as well as improvements 41 00:02:00,469 --> 00:01:58,240 for high-speed transports 42 00:02:02,310 --> 00:02:00,479 particularly in the 43 00:02:04,230 --> 00:02:02,320 approach and landing regime where it 44 00:02:07,190 --> 00:02:04,240 will reduce drag and 45 00:02:08,869 --> 00:02:07,200 therefore require less thrust therefore 46 00:02:10,910 --> 00:02:08,879 produce less noise because the engines 47 00:02:13,830 --> 00:02:10,920 will be at lower power settings 48 00:02:16,070 --> 00:02:13,840 aerodynamic research for airplane wings 49 00:02:20,309 --> 00:02:16,080 is also the goal of another research 50 00:02:24,710 --> 00:02:22,790 using new construction techniques planes 51 00:02:27,110 --> 00:02:24,720 fly through the air easier because they 52 00:02:28,229 --> 00:02:27,120 are built with smoother more aerodynamic 53 00:02:31,190 --> 00:02:28,239 surfaces 54 00:02:34,390 --> 00:02:31,200 as a result planes burn less fuel fly 55 00:02:36,229 --> 00:02:34,400 quieter higher and at faster speeds 56 00:02:39,030 --> 00:02:36,239 in an effort to better understand the 57 00:02:41,270 --> 00:02:39,040 dynamics behind smooth airflow 58 00:02:43,830 --> 00:02:41,280 researchers coat this ultra smooth 59 00:02:50,070 --> 00:02:43,840 highly instrumented learjet wing with an 60 00:02:53,830 --> 00:02:52,949 once airborne pilots target a variety of 61 00:02:56,309 --> 00:02:53,840 allies 62 00:02:58,949 --> 00:02:56,319 and maneuvers designated by aerospace 63 00:03:01,589 --> 00:02:58,959 engineer cindy lee who sits in the back 64 00:03:02,869 --> 00:03:01,599 making real-time analysis of flow fields 65 00:03:05,190 --> 00:03:02,879 over the wing 66 00:03:07,430 --> 00:03:05,200 cindy can also tell by looking at color 67 00:03:10,309 --> 00:03:07,440 shifts in the liquid crystal whether the 68 00:03:12,630 --> 00:03:10,319 airflow is smooth or turbulent she is 69 00:03:14,470 --> 00:03:12,640 piecing together a series of calibrated 70 00:03:17,030 --> 00:03:14,480 measurements that may someday help 71 00:03:20,550 --> 00:03:17,040 aircraft manufacturers design more 72 00:03:26,390 --> 00:03:23,910 nasa's aeronautical research fine-tuning