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Wright Flyer Wind Tunnel Test Data

Actual Data made available for the first time by NASA Quest

KEY:

Alpha = Angle of Attack in degrees (+ nose up)

Lift, w = Lift Force in wind axis in pounds

Drag, w = Drag Force in wind axis in pounds

CL,w = Lift Coefficient

CD,w = Drag Coefficient

L/D = Lift to Drag Ratio

NASA Ames 40 X 80 Foot Wind Tunnel

This data was collected on March 16, 1999 between 5-6:30 p.m.These runs were taken with the engine off. A more complete set of this data is available.



Note:This data is preliminary data. NASA reserves the right to make changes to the data as the result of further analysis and reduction. Any conclusions derived from these data are not endorsed by NASA.

Run # Point # Alpha Lift, w Drag, w CL, w CD, w L/D
43 1 -0.002 0 0 0 0 NaN
43 2 -0.002 0 0 0 0 NaN
43 3 -0.002 -0.493 10.374 -241.7 5085.4 -0.061
43 4 -0.002 637.9 126.78 0.644 0.128 5.506
43 5 -4.001 326.72 108.69 0.3274 0.1089 3.1078
43 6 -1.999 501.53 113.76 0.4943 0.1121 4.7027
43 7 -1.999 513.84 113.4 0.5088 0.1123 4.849
43 8 0.0006 667.28 125.54 0.6711 0.1263 5.8659
43 9 1.9998 812.15 143.15 0.8102 0.1428 6.4151
43 10 3.9844 939.25 167.53 0.9369 0.1671 6.4306
43 11 5.9992 1053.2 196.86 1.0878 0.2033 6.2076
43 12 0.0006 677.65 125.77 0.6728 0.1249 5.9556
44 1 0.0006 650.52 117.25 0.6482 0.1168 6.1334
44 2 -4.001 327.87 107.79 0.3264 0.1073 3.146
44 3 -1.999 474.87 109.7 0.4729 0.1092 4.6033
44 4 -9E-04 639.43 117.24 0.6392 0.1172 6.0127
44 5 1.9983 781.23 133.15 0.7713 0.1315 6.6302
44 6 3.9991 915.91 156.57 0.9235 0.1579 6.7413
44 7 5.9985 1044.6 186.31 1.0473 0.1868 6.5221
44 8 0.0006 644.5 117.09 0.6334 0.1151 6.0695

Last Updated on 3/24/99


 
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