| 000 | 00901pam 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-4909]: Effects of angle of attack and bluntness on the shock-layer properties of a 15 degree cone at a mach number of 10.6 _cJoseph W. Cleary |
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| 260 |
_bNASA _c1968 _aWashington |
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| 300 | _a38p | ||
| 440 | _aNational Aeronautics and Space Administration | ||
| 440 | _aNASA Technical Note | ||
| 500 | _aBound together NASA TN D-4900 to 4910 | ||
| 500 | _aBound vol. Acc. No. 101121 contains Acc. No. TR13259 to TR13268 | ||
| 650 | _aAeronautics | ||
| 650 | _aAircraft -- Conical bodies -- Flow distribution | ||
| 653 | _aAircraft -- Shock layers -- Angle of attack and bluntness | ||
| 700 | _aCleary, Joseph W. | ||
| 942 | _cBK | ||
| 999 |
_c398981 _d398981 |
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