| 000 | 00671pam a2200181a 44500 | ||
|---|---|---|---|
| 005 | 20200624114709.0 | ||
| 008 | 200624b xxu||||| |||| 00| 0 eng d | ||
| 040 | _cIIT Kanpur | ||
| 041 | _aeng | ||
| 100 | _aKehlet, Alan B. | ||
| 245 | 1 |
_aAerodynamic characteristics over a mach number range of 1.40 to 2.78 of a rocket -propelled airplane configuration having a low 52.5 (degree) delta wing and an unswept horizontal tail [NASA TN D-836] _cAlen B. Kehlet |
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| 260 |
_bNasa _c1961 _a Washington, D.C. |
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| 300 | _a26p | ||
| 440 | _aNational Aeronautics and Space Administration (NASA) | ||
| 505 | _aNASA technical report | ||
| 650 | _aAerodynamic | ||
| 942 | _cBK | ||
| 999 |
_c399904 _d399904 |
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