| 000 | 00639nam a22001937a 4500 | ||
|---|---|---|---|
| 003 | OSt | ||
| 005 | 20220103144140.0 | ||
| 008 | 220103b xxu||||| |||| 00| 0 eng d | ||
| 040 | _cIIT Kanpur | ||
| 041 | _aeng | ||
| 100 | _aSpreiter, John R. | ||
| 245 |
_aSlender body theory based on approximate solution of the transonic flow equation [NASA R-2] _cJohn R. Sprieter and Alberta Y. Alksne |
||
| 260 |
_aWashington, D. C. _bNational Aeronautics and Space Administration _c1959 |
||
| 300 | _a54p | ||
| 440 | _aNational Aeronautics and Space Administration | ||
| 650 | _aTransonic flow | ||
| 700 | _aAlksne, Alberta Y. | ||
| 942 | _cREF | ||
| 999 |
_c565281 _d565281 |
||