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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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