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101 0 $aeng
135   $aurun||||a|a||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aLee-side flow over delta wings at supersonic speeds /$fDavid S. Miller and Richard M. Wood
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration, Scientific and Technical Information Branch,$dJune 1985.
215   $a1 online resource (iii, 150 pages) $cillustrations
225 1 $aNASA/TP ;$v2430
300   $a"June 1985."
300   $aPrepared at Langley Research Center.
320   $aIncludes bibliographical references (page 150).
606   $aDelta wings$2nasat
606   $aFlow characteristics$2nasat
606   $aLeading edges$2nasat
606   $aFlow visualization$2nasat
606   $aPressure measurement$2nasat
606   $aAerodynamics, Supersonic
606   $aAirplanes$xWings, Triangular
606   $aVortex-motion
606   $aLeading edges (Aerodynamics)
606   $aAerodynamics, Supersonic$2fast
606   $aAirplanes$xWings, Triangular$2fast
606   $aLeading edges (Aerodynamics)$2fast
606   $aVortex-motion$2fast
615  7$aDelta wings.
615  7$aFlow characteristics.
615  7$aLeading edges.
615  7$aFlow visualization.
615  7$aPressure measurement.
615  0$aAerodynamics, Supersonic.
615  0$aAirplanes$xWings, Triangular.
615  0$aVortex-motion.
615  0$aLeading edges (Aerodynamics)
615  7$aAerodynamics, Supersonic.
615  7$aAirplanes$xWings, Triangular.
615  7$aLeading edges (Aerodynamics)
615  7$aVortex-motion.
700   $aMiller$b David S.$01414616
702   $aWood$b Richard M.
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$bOCLCQ
801  2$bOCLCF
801  2$bOCLCQ
801  2$bOCLCO
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910709793003321
996   $aLee-side flow over delta wings at supersonic speeds$93514463
997   $aUNINA