| 000 | 00849pam 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-382]: Effect of blade cutout on power required by helicopters operating at high tip-speed ratios _cAlfred Gessow and F. B. Gustafson |
|
| 260 |
_bNASA _c1960 _aWashington |
||
| 300 | _a18p | ||
| 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 design, testing and performance | ||
| 700 | _aGessow, Alfred | ||
| 700 | _aGustafson, F. B. | ||
| 942 | _cBK | ||
| 999 |
_c400137 _d400137 |
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