| 000 | 00916pam a2200241a 44500 | ||
|---|---|---|---|
| 003 | OSt | ||
| 040 | _cIIT Kanpur | ||
| 041 | _aeng | ||
| 110 | _aWashington. National Aeronautics and Space Administration (NASA) | ||
| 245 | 1 |
_aNASA Technical Note [NASA TN D-2550]: Application of generalized Newtonian theory to three-dimensional sharp-nose shock-detached bodies at mach for angles of attack up to 25 [degree] _cGeorge C. Ashby and Theodore J. Goldberg |
|
| 260 |
_bNASA _c1965 _aWashington |
||
| 300 | _a41p | ||
| 440 | _aNational Aeronautics and Space Administration | ||
| 440 | _aNASA Technical Note | ||
| 500 | _aBound together NASA TN D-2541 to 2550 | ||
| 500 | _aBound vol. Acc. No. 67642 contains Acc. No. TR9902 to TR9910 | ||
| 650 | _aAerodynamics | ||
| 650 | _aNewtonian theory | ||
| 650 | _aHypersonic flow | ||
| 700 | _aAshby, George C. | ||
| 700 | _aGoldberg, Theodore J. | ||
| 942 | _cBK | ||
| 999 |
_c394103 _d394103 |
||