NASA Technical Paper 2256 - CAFE Foundation
NASA Technical Paper 2256 - CAFE Foundation
NASA Technical Paper 2256 - CAFE Foundation
Create successful ePaper yourself
Turn your PDF publications into a flip-book with our unique Google optimized e-Paper software.
3O<br />
Airplane<br />
VariEze in<br />
flight<br />
Long-Ez<br />
VariEze -in<br />
£unne I<br />
Cessna P-210<br />
Bellanca<br />
Skyrocket II<br />
Gates Learjet<br />
Model 28/29<br />
Longhorn<br />
APPENDIX<br />
TABLE AI o- SUMMARY OF INDICATED WAVINESS MEASURED ON TEST AIRPLANES<br />
Surface I]<br />
Right wing 0.25<br />
,40<br />
.55<br />
.85<br />
.95<br />
Right win@let O. 55<br />
Right wing O. 55<br />
.85<br />
Right wingle£ 0.55<br />
Right canard 0.45<br />
i<br />
Right ,¢ing O. 25<br />
.55<br />
.75<br />
Right winglet 0.25<br />
.80<br />
0.S. - pr0ductiSn<br />
u.s. - filled and sanded<br />
L.S. - filled and sanded<br />
Inboard wake probe<br />
Outboard wake probe<br />
Right wing<br />
Right winglet<br />
Upper<br />
Lower<br />
Upper<br />
Lower<br />
0.48<br />
.72<br />
0.10<br />
.63<br />
Largest wave measured<br />
Position,<br />
s/c<br />
O. 736<br />
.309<br />
.578<br />
.704<br />
.535<br />
0.678<br />
0.189<br />
.208<br />
0.270<br />
o 356<br />
0.333<br />
.433<br />
.511<br />
0.223<br />
.533<br />
0.2?8<br />
.095<br />
.125<br />
0.312<br />
.065<br />
0.065<br />
.065<br />
0.430<br />
.450<br />
0.17<br />
.69<br />
k, in.<br />
2.0<br />
2.0<br />
2.0<br />
2.0<br />
2.0<br />
2.0<br />
2.0<br />
2.0<br />
3.0<br />
1.75<br />
2.0<br />
2.5<br />
2.0<br />
2.0<br />
• 3.25<br />
3.5<br />
2.0<br />
3.5<br />
2.0<br />
2.0<br />
2.0-<br />
2.0<br />
2.0<br />
3.0<br />
2.0<br />
2.0<br />
h/k<br />
0.0035<br />
.0060<br />
.0030<br />
.0075<br />
.0030<br />
O.0O7O<br />
0.0030<br />
.0020<br />
0.0020<br />
0.0046<br />
0.00_5<br />
.0024<br />
.0030<br />
0.0045<br />
.0018<br />
0.0020<br />
.0050<br />
.0011<br />
0_0015<br />
.0075<br />
0.0045<br />
.0070<br />
0.0020<br />
.0030<br />
0.0135<br />
.0010<br />
Largest wave measured<br />
in laminar region<br />
Positioni"I<br />
s/c<br />
k, in. h/k<br />
0.194 3.0 0.0030 0.0100<br />
.309 2.0 .0060 .0100<br />
.316 3.0 .0020 .0105<br />
.477 4.0- .0015 .0115<br />
.347 2.0 .0020 .0120<br />
0,465 3.5 0.0017 0.0125<br />
.189 2.0 0.0030 0.0100<br />
•208 2.0 .0020 o0110<br />
0.270 3.0 0.0020 0.0115<br />
0.356 1.75 0;0046 0.0135<br />
0.333 2.0 0.004[ O.0180<br />
.433 2.5 .0024 .0193<br />
.511 2.0 .0030 .020_<br />
0.223 2.0 0.0045 0.0215<br />
.533 3.25 .0018 .0248<br />
0.228 3.5 0.0020 " 0.0100<br />
• 095 2.0 .0050 .0100<br />
,1 25 3.5 .0011 .0100<br />
0,312 2.0 0.0015 0.0078<br />
•065 2.0 .0075 .0078<br />
0,065 2.0 0.0045 O.0079<br />
,065 2.0 .0070 .0079<br />
i ',.<br />
0.10 2.0 0.0010 0.0040<br />
.0041<br />
0,17 2.0 0.0135 0.0050<br />
.0070<br />
®
Change language