LEADER 01460oam  2200433   450 
001 9910716585903321
005 20210608120507.0
035   $a(CKB)5470000002522293
035   $a(OCoLC)890694822
035   $a(OCoLC)995470000002522293
035   $a(EXLCZ)995470000002522293
100   $a20140916j197305    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aLocal flow measurement at the inlet spike tip of a mach 3 supersonic cruise airplane /$fby Harold J. Johnson and Earl J. Montoya
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dMay 1973.
215   $a1 online resource (40 pages) $cillustrations
225 1 $aNASA/TN ;$vD-6987
300   $a"May 1973."
320   $aIncludes bibliographical references (pages 15).
606   $aMach number$2nasat
606   $aFlight tests$2nasat
606   $aWind tunnel tests$2nasat
615  7$aMach number.
615  7$aFlight tests.
615  7$aWind tunnel tests.
700   $aJohnson$b Harold J.$01402444
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910716585903321
996   $aLocal flow measurement at the inlet spike tip of a mach 3 supersonic cruise airplane$93472917
997   $aUNINA