000 | 00850pam 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-2935]: Study of gas injection in the boundary layer of a hypersonic wind tunnel to extend the useful operating range _cJohn B. McDevitt |
|
260 |
_aWashington _bNASA _c1965 |
||
300 | _a33p | ||
440 | _aNational Aeronautics and Space Administration | ||
440 | _aNASA Technical Note | ||
500 | _aBound together NASA TN D-2931 to 2940 | ||
500 | _aBound vol. Acc. No. 64293 contains Acc. No. TR9785 to TR9793 | ||
650 | _aFacilities, research and support | ||
650 | _aHypersonic wind tunnel | ||
650 | _aGas injection scheme | ||
700 | _aMcDevitt, John B. | ||
942 | _cBK | ||
999 |
_c406225 _d406225 |