000 00730nam a22002057a 4500
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040 _cIIT Kanpur
041 _aeng
110 _aDustin, Miles O.
245 _aContinuoous output tremiminal shock mixed compression inlets evaluated in wind tunnel tests of YF-12 aircfaft inlet [NASA TM X-3144]
_bNational Aeronautics and Space Administration
_cMiles O. Dustin, Gary L. Cole and George H. Neiner
260 _aWashington, D. C.
_bOhio
_c1974
300 _a23p
440 _aNational Aeronautics and Space Administration (NASA)
650 _aWind tunnel
700 _aCole, Gary L.
700 _aNeiner, George H.
942 _cREF
999 _c564476
_d564476