1 00:00:11,360 --> 00:00:13,910 since its introduction three decades ago 2 00:00:13,910 --> 00:00:13,920 since its introduction three decades ago 3 00:00:13,920 --> 00:00:15,829 since its introduction three decades ago the helicopter has been a valuable 4 00:00:15,829 --> 00:00:15,839 the helicopter has been a valuable 5 00:00:15,839 --> 00:00:19,510 the helicopter has been a valuable national asset 6 00:00:19,510 --> 00:00:19,520 7 00:00:19,520 --> 00:00:21,670 more recently the tilt rotor aircraft 8 00:00:21,670 --> 00:00:21,680 more recently the tilt rotor aircraft 9 00:00:21,680 --> 00:00:23,349 more recently the tilt rotor aircraft has demonstrated it can do almost 10 00:00:23,349 --> 00:00:23,359 has demonstrated it can do almost 11 00:00:23,359 --> 00:00:26,230 has demonstrated it can do almost everything the helicopter does and more 12 00:00:26,230 --> 00:00:26,240 everything the helicopter does and more 13 00:00:26,240 --> 00:00:28,790 everything the helicopter does and more including flying like a fixed-wing plane 14 00:00:28,790 --> 00:00:28,800 including flying like a fixed-wing plane 15 00:00:28,800 --> 00:00:32,229 including flying like a fixed-wing plane once airborne 16 00:00:32,229 --> 00:00:32,239 17 00:00:32,239 --> 00:00:34,229 as our airports and air space become 18 00:00:34,229 --> 00:00:34,239 as our airports and air space become 19 00:00:34,239 --> 00:00:36,310 as our airports and air space become more congested and the demand for 20 00:00:36,310 --> 00:00:36,320 more congested and the demand for 21 00:00:36,320 --> 00:00:38,709 more congested and the demand for short-range commuter flights grows the 22 00:00:38,709 --> 00:00:38,719 short-range commuter flights grows the 23 00:00:38,719 --> 00:00:41,510 short-range commuter flights grows the appeal of rotorcraft is becoming greater 24 00:00:41,510 --> 00:00:41,520 appeal of rotorcraft is becoming greater 25 00:00:41,520 --> 00:00:43,990 appeal of rotorcraft is becoming greater but current systems are too noisy burn 26 00:00:43,990 --> 00:00:44,000 but current systems are too noisy burn 27 00:00:44,000 --> 00:00:46,310 but current systems are too noisy burn too much fuel and require expensive 28 00:00:46,310 --> 00:00:46,320 too much fuel and require expensive 29 00:00:46,320 --> 00:00:47,270 too much fuel and require expensive maintenance 30 00:00:47,270 --> 00:00:47,280 maintenance 31 00:00:47,280 --> 00:00:49,590 maintenance it is problems like these which nasa's 32 00:00:49,590 --> 00:00:49,600 it is problems like these which nasa's 33 00:00:49,600 --> 00:00:51,350 it is problems like these which nasa's ames research center in mountain view 34 00:00:51,350 --> 00:00:51,360 ames research center in mountain view 35 00:00:51,360 --> 00:00:53,830 ames research center in mountain view california is studying 36 00:00:53,830 --> 00:00:53,840 california is studying 37 00:00:53,840 --> 00:00:56,150 california is studying here engineers use wind tunnels to carry 38 00:00:56,150 --> 00:00:56,160 here engineers use wind tunnels to carry 39 00:00:56,160 --> 00:00:58,790 here engineers use wind tunnels to carry out aerodynamic tests similar to those 40 00:00:58,790 --> 00:00:58,800 out aerodynamic tests similar to those 41 00:00:58,800 --> 00:01:00,470 out aerodynamic tests similar to those done on conventional planes and 42 00:01:00,470 --> 00:01:00,480 done on conventional planes and 43 00:01:00,480 --> 00:01:01,910 done on conventional planes and automobiles 44 00:01:01,910 --> 00:01:01,920 automobiles 45 00:01:01,920 --> 00:01:03,830 automobiles a rotor blade section is mounted in 46 00:01:03,830 --> 00:01:03,840 a rotor blade section is mounted in 47 00:01:03,840 --> 00:01:05,590 a rotor blade section is mounted in front of a sophisticated instrument 48 00:01:05,590 --> 00:01:05,600 front of a sophisticated instrument 49 00:01:05,600 --> 00:01:09,510 front of a sophisticated instrument called a laser velocimeter or lv 50 00:01:09,510 --> 00:01:09,520 called a laser velocimeter or lv 51 00:01:09,520 --> 00:01:12,390 called a laser velocimeter or lv once setup is complete air along with a 52 00:01:12,390 --> 00:01:12,400 once setup is complete air along with a 53 00:01:12,400 --> 00:01:14,630 once setup is complete air along with a fine oil mist is blown through the 54 00:01:14,630 --> 00:01:14,640 fine oil mist is blown through the 55 00:01:14,640 --> 00:01:15,750 fine oil mist is blown through the tunnel 56 00:01:15,750 --> 00:01:15,760 tunnel 57 00:01:15,760 --> 00:01:18,070 tunnel tiny oil particles reflect light back 58 00:01:18,070 --> 00:01:18,080 tiny oil particles reflect light back 59 00:01:18,080 --> 00:01:19,270 tiny oil particles reflect light back into the air 60 00:01:19,270 --> 00:01:19,280 into the air 61 00:01:19,280 --> 00:01:21,350 into the air allowing researchers to determine how 62 00:01:21,350 --> 00:01:21,360 allowing researchers to determine how 63 00:01:21,360 --> 00:01:23,670 allowing researchers to determine how fast air flows around any area of the 64 00:01:23,670 --> 00:01:23,680 fast air flows around any area of the 65 00:01:23,680 --> 00:01:26,710 fast air flows around any area of the blade being tested 66 00:01:26,710 --> 00:01:26,720 blade being tested 67 00:01:26,720 --> 00:01:28,630 blade being tested related work is underway at the ames 68 00:01:28,630 --> 00:01:28,640 related work is underway at the ames 69 00:01:28,640 --> 00:01:31,429 related work is underway at the ames outdoor aerodynamic research facility 70 00:01:31,429 --> 00:01:31,439 outdoor aerodynamic research facility 71 00:01:31,439 --> 00:01:33,590 outdoor aerodynamic research facility in this particular study engineers are 72 00:01:33,590 --> 00:01:33,600 in this particular study engineers are 73 00:01:33,600 --> 00:01:35,910 in this particular study engineers are investigating how certain aerodynamic 74 00:01:35,910 --> 00:01:35,920 investigating how certain aerodynamic 75 00:01:35,920 --> 00:01:37,749 investigating how certain aerodynamic characteristics of rotor systems 76 00:01:37,749 --> 00:01:37,759 characteristics of rotor systems 77 00:01:37,759 --> 00:01:40,630 characteristics of rotor systems influence overall performance according 78 00:01:40,630 --> 00:01:40,640 influence overall performance according 79 00:01:40,640 --> 00:01:42,069 influence overall performance according to the chief of the rotary wing 80 00:01:42,069 --> 00:01:42,079 to the chief of the rotary wing 81 00:01:42,079 --> 00:01:44,950 to the chief of the rotary wing aeromechanics branch at ames ten percent 82 00:01:44,950 --> 00:01:44,960 aeromechanics branch at ames ten percent 83 00:01:44,960 --> 00:01:46,950 aeromechanics branch at ames ten percent of a rotor system's total energy is 84 00:01:46,950 --> 00:01:46,960 of a rotor system's total energy is 85 00:01:46,960 --> 00:01:49,749 of a rotor system's total energy is wasted because downward forces generated 86 00:01:49,749 --> 00:01:49,759 wasted because downward forces generated 87 00:01:49,759 --> 00:01:51,990 wasted because downward forces generated by the spinning blades push other parts 88 00:01:51,990 --> 00:01:52,000 by the spinning blades push other parts 89 00:01:52,000 --> 00:01:54,550 by the spinning blades push other parts of the aircraft towards the ground bill 90 00:01:54,550 --> 00:01:54,560 of the aircraft towards the ground bill 91 00:01:54,560 --> 00:01:55,670 of the aircraft towards the ground bill warnbrook 92 00:01:55,670 --> 00:01:55,680 warnbrook 93 00:01:55,680 --> 00:01:57,270 warnbrook consequently the rotor system has to 94 00:01:57,270 --> 00:01:57,280 consequently the rotor system has to 95 00:01:57,280 --> 00:01:59,030 consequently the rotor system has to work 10 96 00:01:59,030 --> 00:01:59,040 work 10 97 00:01:59,040 --> 00:01:59,990 work 10 harder 98 00:01:59,990 --> 00:02:00,000 harder 99 00:02:00,000 --> 00:02:02,709 harder to develop an equivalent amount of lift 100 00:02:02,709 --> 00:02:02,719 to develop an equivalent amount of lift 101 00:02:02,719 --> 00:02:04,389 to develop an equivalent amount of lift say to lift 102 00:02:04,389 --> 00:02:04,399 say to lift 103 00:02:04,399 --> 00:02:07,510 say to lift a crew and useful cargo complementing 104 00:02:07,510 --> 00:02:07,520 a crew and useful cargo complementing 105 00:02:07,520 --> 00:02:09,589 a crew and useful cargo complementing these experimental studies are computer 106 00:02:09,589 --> 00:02:09,599 these experimental studies are computer 107 00:02:09,599 --> 00:02:12,229 these experimental studies are computer simulations when a blade rotates it is 108 00:02:12,229 --> 00:02:12,239 simulations when a blade rotates it is 109 00:02:12,239 --> 00:02:14,470 simulations when a blade rotates it is constantly colliding with tornado-like 110 00:02:14,470 --> 00:02:14,480 constantly colliding with tornado-like 111 00:02:14,480 --> 00:02:16,790 constantly colliding with tornado-like pockets of turbulence created by other 112 00:02:16,790 --> 00:02:16,800 pockets of turbulence created by other 113 00:02:16,800 --> 00:02:19,430 pockets of turbulence created by other blades in front of it the result is less 114 00:02:19,430 --> 00:02:19,440 blades in front of it the result is less 115 00:02:19,440 --> 00:02:21,589 blades in front of it the result is less efficiency and greater noise 116 00:02:21,589 --> 00:02:21,599 efficiency and greater noise 117 00:02:21,599 --> 00:02:24,390 efficiency and greater noise simulations like these cut costs by 118 00:02:24,390 --> 00:02:24,400 simulations like these cut costs by 119 00:02:24,400 --> 00:02:25,990 simulations like these cut costs by allowing researchers to study 120 00:02:25,990 --> 00:02:26,000 allowing researchers to study 121 00:02:26,000 --> 00:02:28,550 allowing researchers to study aerodynamic problems before building the 122 00:02:28,550 --> 00:02:28,560 aerodynamic problems before building the 123 00:02:28,560 --> 00:02:31,670 aerodynamic problems before building the final aircraft 124 00:02:31,670 --> 00:02:31,680 125 00:02:31,680 --> 00:02:34,470 nasa's rotorcraft research an approach 126 00:02:34,470 --> 00:02:34,480 nasa's rotorcraft research an approach 127 00:02:34,480 --> 00:02:36,470 nasa's rotorcraft research an approach aimed at improving the performance of 128 00:02:36,470 --> 00:02:36,480 aimed at improving the performance of 129 00:02:36,480 --> 00:02:40,599 aimed at improving the performance of future transport systems