| 000 | 00744pam a2200205a 44500 | ||
|---|---|---|---|
| 003 | OSt | ||
| 005 | 20220902121455.0 | ||
| 008 | 220902b xxu||||| |||| 00| 0 eng d | ||
| 040 | _cIIT Kanpur | ||
| 041 | _aeng | ||
| 100 | _aJackson, Charlie M. | ||
| 245 | 1 |
_aA SEMIGRAPHICAL METHOD OF APPLYING IMPACT THEORY TO AN ARBITRARY BODY TO OBTAIN THE HYPERSONIC AERODYNAMIC CHARACTERISTICS AT ANGLE OF ATTACK AND SIDESLIP [NASA TN D-795] _cCharlie M. Jackson |
|
| 260 |
_bNational Aeronautics and Space Administration _c1961 _aWashington, D.C. |
||
| 300 | _a18p | ||
| 440 | _aNational Aeronautics and Space Administration | ||
| 440 | _aNASA Technical Note | ||
| 500 | _aBound With NASA TN D 791-800 | ||
| 650 | _aArbitrary body | ||
| 942 | _cTR | ||
| 999 |
_c394254 _d394254 |
||