| 000 | 01055pam a2200253a 44500 | ||
|---|---|---|---|
| 003 | OSt | ||
| 040 | _cIIT Kanpur | ||
| 041 | _aeng | ||
| 110 | _aWashington. National Aeronautics and Space Administration (NASA) | ||
| 245 | 1 |
_aNASA Technical Note [NASA TN D-5272]: An experimental and theoretical investigation of a symmetrical and a cambered delta wing configuration at mach numbers from 2.0 to 10.7 _cWalter P. Nelms, Ralph L. Carmichael and Charles R. Castellano |
|
| 260 |
_bNASA _c1969 _aWashington |
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| 300 | _a31p | ||
| 440 | _aNational Aeronautics and Space Administration | ||
| 440 | _aNASA Technical Note | ||
| 500 | _aBound together NASA TN D-5271 to 5280 | ||
| 500 | _aBound vol. Acc. No. 101151 contains Acc. No. TR7891 to TR7899 | ||
| 650 | _aAeronautics | ||
| 650 | _aSpacecraft -- Airplane -- Wing body configuration -- Camber effects | ||
| 650 | _aAirplane -- Wing body configuration -- Camber effects | ||
| 700 | _aNelms, Walter P. | ||
| 700 | _aCarmichael, Ralph L. | ||
| 700 | _aCastellano, Charles R. | ||
| 942 | _cBK | ||
| 999 |
_c393730 _d393730 |
||