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