| 000 | 00830pam 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-545]: A note on the drag due to lift of delta wings at mach numbers up to 2.0 _cby Robert S. Osborne and Thomas C. Kelly |
|
| 260 |
_bNASA _c1960 _aWashington |
||
| 300 | _a14p | ||
| 440 | _aNational Aeronautics and Space Administration | ||
| 440 | _aNASA Technical Note | ||
| 500 | _aBound together NASA TN D-541 to 550 | ||
| 500 | _aBound vol. Acc. No. 65466 contains Acc. No. TR15854 to TR15862 | ||
| 650 | _aAircraft stability and control | ||
| 650 | _aAerodynamics, Aircraft | ||
| 700 | _aOsborne, Robert S. | ||
| 700 | _aKelly, Thomas C. | ||
| 942 | _cBK | ||
| 999 |
_c399461 _d399461 |
||