| 000 | 00710 a2200157 4500 | ||
|---|---|---|---|
| 005 | 20221215114050.0 | ||
| 100 | _aRobinson, Ross B. | ||
| 245 | 1 |
_aNASA Memo [10-2-58L] _bAERODYNAMIC CHARACTERISTICS FOR COMBINED ANGLES OF ATTACK AND SIDESLIP OF A LOW-ASPECT-RATIO CRUCIFORM-WING MISSILE CONFIGURATION EMPLOYING VARIOUS CANARD AND TRAILING-EDGE FLAP CONTROLS AT A NO.2.01 _cRoss B. Robinson and M. Leroy Spearman |
|
| 260 |
_aWashington _bNational Aeronautics and Space Administration _c1958 |
||
| 300 | _a71p | ||
| 440 | _aNASA Memorandum | ||
| 500 | _aNASA Memorandum 10-1-58L-10-17-58L Bound Vol. No.102461; Contents: TR-8572-8580 | ||
| 650 | _aAerodynamics | ||
| 700 | _aSpearman, M. Leroy | ||
| 942 | _cTR | ||
| 999 |
_c393963 _d393963 |
||