LEADER 01837nam  2200469   450 
001 9910709981303321
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035   $a(EXLCZ)995470000002474451
100   $a20180822j198507    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aExperimental and theoretical study of the longitudinal aerodynamic characteristics of delta and double-delta wings at mach numbers of 1.60, 1.90, and 2.16 /$fRichard M. Wood and Peter F. Covell
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration, Scientific and Technical Information Branch,$dJuly 1985.
215   $a1 online resource (119 pages, 1 unnumbered page) $cillustrations
225 1 $aNASA/TP ;$v2433
300   $a"July 1985."
320   $aIncludes bibliographical references (page 119).
606   $aDelta wings$2nasat
606   $aSupersonic airfoils$2nasat
606   $aMach number$2nasat
606   $aSweptback wings$2nasat
606   $aSupersonic flow$2nasat
615  7$aDelta wings.
615  7$aSupersonic airfoils.
615  7$aMach number.
615  7$aSweptback wings.
615  7$aSupersonic flow.
700   $aWood$b Richard M.$0144306
702   $aCovell$b Peter F.
712 02$aUnited States.$bNational Aeronautics and Space Administration.$bScientific and Technical Information Branch,
712 02$aLangley Research Center.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910709981303321
996   $aExperimental and theoretical study of the longitudinal aerodynamic characteristics of delta and double-delta wings at mach numbers of 1.60, 1.90, and 2.16$93473802
997   $aUNINA