| 000 | 00617pam a2200181a 44500 | ||
|---|---|---|---|
| 005 | 20200624121132.0 | ||
| 008 | 200624b xxu||||| |||| 00| 0 eng d | ||
| 040 | _cIIT Kanpur | ||
| 041 | _aeng | ||
| 100 | _aSpearman, M. Leroy | ||
| 245 | 1 |
_aAerodynamic characteristics in pitch of a series of cruciform-wing missiles with canard controls at a mach number of 2.01 [NASA TN D-839] _cM. Leroy Spearman |
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| 260 |
_bNasa _c1961 _a Washington, D.C. |
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| 300 | _a40p | ||
| 440 | _aNational Aeronautics and space Administratio (NASA) | ||
| 505 | _aNASA technical report | ||
| 650 | _acruciform-wing | ||
| 942 | _cBK | ||
| 999 |
_c399907 _d399907 |
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