| 000 | 00685nam a2200193 4500 | ||
|---|---|---|---|
| 005 | 20200810102828.0 | ||
| 008 | 200810b xxu||||| |||| 00| 0 eng d | ||
| 040 | _cIIT Kanpur | ||
| 041 | _aeng | ||
| 100 | _aWilbur, D. Middleton | ||
| 245 |
_aA numerical method for calculating the flat-plate pressure distribution on supersonic wings of supersonic wings of arbitrary planform. [NASA TN D-2570] _cWilbur D. Middleton and Harry W. Carlson |
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| 260 |
_aWashington, D. C _bNASA _c1965 |
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| 300 | _a23p | ||
| 440 | _aNational Aeronautics and Space Administration (NASA) | ||
| 505 | _aNASA technical report | ||
| 650 | _aArbitrary | ||
| 700 | _aCarlson, Harry W. | ||
| 942 | _cTR | ||
| 999 |
_c563321 _d563321 |
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