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100   $a19910326j197212    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aEffect of wing sweep, angle of attack, Reynolds number, and wing root fillet on the interference heating to the wing windward surface of an entry vehicle configuration /$fby Louis E. Clark
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dDecember 1972.
215   $a1 online resource (52 pages) $cillustrations
225 1 $aNASA/TN ;$vD-7060
300   $a"December 1972."
320   $aIncludes bibliographical references (page 10).
606   $aAerospace vehicles$2nasat
606   $aAerodynamics$2nasat
606   $aSpace vehicles$xAtmospheric entry
606   $aLeading edges (Aerodynamics)
606   $aAerodynamic heating
606   $aAerothermodynamics
606   $aSpace shuttles
606   $aAerodynamic heating$2fast
606   $aAerothermodynamics$2fast
606   $aLeading edges (Aerodynamics)$2fast
606   $aSpace shuttles$2fast
606   $aSpace vehicles$xAtmospheric entry$2fast
615  7$aAerospace vehicles.
615  7$aAerodynamics.
615  0$aSpace vehicles$xAtmospheric entry.
615  0$aLeading edges (Aerodynamics)
615  0$aAerodynamic heating.
615  0$aAerothermodynamics.
615  0$aSpace shuttles.
615  7$aAerodynamic heating.
615  7$aAerothermodynamics.
615  7$aLeading edges (Aerodynamics)
615  7$aSpace shuttles.
615  7$aSpace vehicles$xAtmospheric entry.
700   $aClark$b Louis E.$01419962
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bABC
801  1$bABC
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801  2$bOCLCE
801  2$bOCLCQ
801  2$bOCLCF
801  2$bOCLCQ
801  2$bOCLCO
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910716019303321
996   $aEffect of wing sweep, angle of attack, Reynolds number, and wing root fillet on the interference heating to the wing windward surface of an entry vehicle configuration$93536156
997   $aUNINA