LEADER 01974oam  2200589   450 
001 9910715170603321
005 20201211125543.0
035   $a(CKB)5470000002508306
035   $a(OCoLC)761497571
035   $a(EXLCZ)995470000002508306
100   $a20111115j196808    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aEffect of hinge-line bleed on heat transfer and pressure distribution over a wedge-flap combination at Mach 10.4 /$fby H. Harris Hamilton, and J. David Dearing
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dAugust 1968.
215   $a1 online resource (44 pages) $cillustrations
225 1 $aNASA technical note ;$vTN D-4686
300   $a"August 1968."
320   $aIncludes bibliographical references (pages 18-21).
606   $aBoundary layer control
606   $aFlaps (Airplanes)
606   $aWedges
606   $aAircraft separation
606   $aAircraft separation$2fast
606   $aBoundary layer control$2fast
606   $aFlaps (Airplanes)$2fast
606   $aWedges$2fast
615  0$aBoundary layer control.
615  0$aFlaps (Airplanes)
615  0$aWedges.
615  0$aAircraft separation.
615  7$aAircraft separation.
615  7$aBoundary layer control.
615  7$aFlaps (Airplanes)
615  7$aWedges.
700   $aHamilton$b H. Harris$01405571
702   $aDearing$b J. David
712 02$aUnited States.$bNational Aeronautics and Space Administration,
712 02$aLangley Research Center.
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCQ
801  2$bOCLCF
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910715170603321
996   $aEffect of hinge-line bleed on heat transfer and pressure distribution over a wedge-flap combination at Mach 10.4$93482420
997   $aUNINA