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001 9910716081203321
005 20210504153131.0
035   $a(CKB)5470000002517290
035   $a(OCoLC)1182784765
035   $a(OCoLC)995470000002517290
035   $a(EXLCZ)995470000002517290
100   $a20200806j196901    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aDesign of supersonic inlets by a computer program incorporating the method of characteristics /$fby Bernhard H. Anderson
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dJanuary 1969.
215   $a1 online resource (ii, 115 pages) $cillustrations
225 1 $aNASA/TN ;$vD-4960
300   $a"January 1969."
320   $aIncludes bibliographical references (page 100).
606   $aFORTRAN$2nasat
606   $aJet engines$2nasat
606   $aFORTRAN IV (Computer program language)$2fast
606   $aJet engines$xAir intakes$2fast
615  7$aFORTRAN.
615  7$aJet engines.
615  7$aFORTRAN IV (Computer program language)
615  7$aJet engines$xAir intakes.
700   $aAnderson$b Bernhard H.$01386038
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bCOP
801  1$bCOP
801  2$bOCLCO
801  2$bOCLCF
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910716081203321
996   $aDesign of supersonic inlets by a computer program incorporating the method of characteristics$93453861
997   $aUNINA