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100   $a20111115j198507    ua             0
101 0 $aeng
135   $aurun||||a|a||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aExperimental and theoretical study of 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) $cillustrations
225 1 $aNASA/TP ;$v2433
320   $aIncludes bibliographical references (page 119).
606   $aSupersonic airfoils$2nasat
606   $aDelta wings$2nasat
606   $aSupersonic flow$2nasat
606   $aAerodynamic drag$2nasat
606   $aMach number$2nasat
606   $aAirplanes$xWings, Triangular$xAerodynamics
615  7$aSupersonic airfoils.
615  7$aDelta wings.
615  7$aSupersonic flow.
615  7$aAerodynamic drag.
615  7$aMach number.
615  0$aAirplanes$xWings, Triangular$xAerodynamics.
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$bOCLCE
801  1$bOCLCE
801  2$bOCLCQ
801  2$bOCLCO
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910709794403321
996   $aExperimental and theoretical study of longitudinal aerodynamic characteristics of delta and double-delta wings at Mach numbers of 1.60, 1.90, and 2.16$93504013
997   $aUNINA