| 000 | 00901pam a2200217a 44500 | ||
|---|---|---|---|
| 003 | OSt | ||
| 040 | _cIIT Kanpur | ||
| 041 | _aeng | ||
| 110 | _aWashington. National Aeronautics and Space Administration (NASA) | ||
| 245 | 1 |
_aNASA Technical Note [NASA TN D-387]: Effect of streamline contouring in the wing-fuselage juncture in combination with the supersonic area rule on a sweptback-wing--fuselage configuration of high fineness ratio _cCharles D. Trescot |
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| 260 |
_bNASA _c1960 _aWashington |
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| 300 | _a19p | ||
| 440 | _aNational Aeronautics and Space Administration | ||
| 440 | _aNASA Technical Note | ||
| 500 | _aBound together NASA TN D-381 to 390 | ||
| 500 | _aBound vol. Acc. No. 63662 contains Acc. No. TR15585 to TR15589, TR15610, TR15590 to TR15591 & TR15611 | ||
| 650 | _aAircraft, Fluid mechanics | ||
| 650 | _aFuselages | ||
| 700 | _aTrescot, Charles D. | ||
| 942 | _cBK | ||
| 999 |
_c400143 _d400143 |
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