| 000 | 00629pam a2200193a 44500 | ||
|---|---|---|---|
| 005 | 20200701155608.0 | ||
| 008 | 200701b xxu||||| |||| 00| 0 eng d | ||
| 040 | _cIIT Kanpur | ||
| 041 | _aeng | ||
| 100 | _aKussoy, Marvin | ||
| 245 | 1 |
_aLocal pressure distribution on a blunt delta wing for angles of attack up to 35(degre) at mach numbers of 3.4 and 4.7 [ NASA TN D-1554 ] _cMarvin Kussoy |
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| 260 |
_bNasa _c1962 _aWashington, D.C. |
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| 300 | _a21p | ||
| 440 | _aNational Aeronautics and Space Administration (NASA) | ||
| 505 | _aNASA technical report | ||
| 650 | _aAir jets | ||
| 650 | _aTurbulence | ||
| 942 | _cBK | ||
| 999 |
_c400050 _d400050 |
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