LEADER 01567nam  2200469   450 
001 9910709665303321
005 20180530121237.0
035   $a(CKB)5470000002471582
035   $a(OCoLC)1038017415
035   $a(EXLCZ)995470000002471582
100   $a20180530j198111    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aVORCAM $ea computer program for calculating vortex lift effect of cambered wings by the suction analogy /$fC. Edward Lan and Jen-Fu Chang
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dNovember 1981.
215   $a1 online resource (122 pages) $cillustrations
225 1 $aNASA/CR ;$v165800
300   $a"November 1981."
320   $aIncludes bibliographical references (page 122).
517   $aVORCAM 
606   $aComputer programs$2nasat
606   $aCambered wings$2nasat
606   $aSupersonic flow$2nasat
606   $aUser manuals (computer programs)$2nasat
606   $aSubsonic flow$2nasat
615  7$aComputer programs.
615  7$aCambered wings.
615  7$aSupersonic flow.
615  7$aUser manuals (computer programs)
615  7$aSubsonic flow.
700   $aLan$b C. Edward$g(Chuan-Tau Edward),$f1935-$01411566
702   $aChang$b Jen-Fu
712 02$aLangley Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910709665303321
996   $aVORCAM$93503124
997   $aUNINA