| 000 | 00786pam a2200205a 44500 | ||
|---|---|---|---|
| 003 | OSt | ||
| 005 | 20221227160558.0 | ||
| 008 | 221227b xxu||||| |||| 00| 0 eng d | ||
| 040 | _cIIT Kanpur | ||
| 041 | _aeng | ||
| 100 | _aOlstad,Walter B | ||
| 245 | 1 |
_aTheoretical evaluation of hypersonic forces, moments, and stability derivatives for a combination of flat plates, including effects of blunt leading edges by Newtonian impact theory[NASA TN D-1015] _cWalter B. Olstad |
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| 260 |
_a Washington, D.C. _bNational Aeronautics and Space Administration Washington _c1962 |
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| 300 | _a66p | ||
| 440 | _aNational Aeronaitics and Space Adminstration | ||
| 440 | _aNASA Technical Note | ||
| 500 | _aBound vol. contains D 1011-1020 | ||
| 650 | _aHypersonic forces | ||
| 942 | _cTR | ||
| 999 |
_c394300 _d394300 |
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