| 000 | 00885pam a2200229a 44500 | ||
|---|---|---|---|
| 003 | OSt | ||
| 040 | _cIIT Kanpur | ||
| 041 | _aeng | ||
| 110 | _aWashington. National Aeronautics and Space Administration (NASA) | ||
| 245 | 1 |
_aNASA Technical Note [NASA TN D-5046]: A method for determining the total drag of a pointed body of revolution in supersonic flow with turbulent boundary layer _cCharlie M. Jackson and Rudeen S. Smith |
|
| 260 |
_aWashington _bNASA _c1969 |
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| 300 | _a65p | ||
| 440 | _aNational Aeronautics and Space Administration | ||
| 440 | _aNASA Technical Note | ||
| 500 | _aBound together NASA TN D-5041 to 5050 | ||
| 500 | _aBound vol. Acc. No. 101134 contains Acc. No. TR16875 to TR16883 | ||
| 650 | _aAeronautics | ||
| 650 | _aSupersonic flow -- Drag -- Mathematical model | ||
| 700 | _aJackson, Charlie M. | ||
| 700 | _aSmith, Rudeen S. | ||
| 942 | _cBK | ||
| 999 |
_c402330 _d402330 |
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