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100   $a20120408j196812    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 12$aA mathematical analysis of supersonic inlet dynamics /$fby Ross G. Willoh
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dDecember 1968.
215   $a1 online resource (ii, 41 pages) $cillustrations
225 1 $aNASA/TN ;$vD-4969
300   $a"December 1968."
320   $aIncludes bibliographical references (page 41).
606   $aAerodynamics$2nasat
606   $aAir ducts$2nasat
606   $aApplications of mathematics$2nasat
606   $aAerodynamics, Supersonic
606   $aAerodynamics, Supersonic$2fast
606   $aAir ducts$xAerodynamics$2fast
606   $aAirplanes$xTurbojet engines$xAir intakes$2fast
606   $aMathematical analysis$2fast
615  7$aAerodynamics.
615  7$aAir ducts.
615  7$aApplications of mathematics.
615  0$aAerodynamics, Supersonic.
615  7$aAerodynamics, Supersonic.
615  7$aAir ducts$xAerodynamics.
615  7$aAirplanes$xTurbojet engines$xAir intakes.
615  7$aMathematical analysis.
700   $aWilloh$b Ross G.$01417018
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCQ
801  2$bOCLCF
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910716078003321
996   $aA mathematical analysis of supersonic inlet dynamics$93524084
997   $aUNINA