LEADER 02008oam  2200601   450 
001 9910715018403321
005 20201130132459.0
035   $a(CKB)5470000002507823
035   $a(OCoLC)761173274
035   $a(EXLCZ)995470000002507823
100   $a20111115j196808    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aApplication of the leading-edge-suction analogy of vortex lift to the drag due to lift of sharp-edge delta wings /$fby Edward C. Polhamus
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dAugust 1968.
215   $a1 online resource (14 pages) $cillustrations
225 1 $aNASA technical note ;$vTN D-4739
300   $a"August 1968."
320   $aIncludes bibliographical references (page 8).
606   $aDelta wing airplanes
606   $aVortex flaps
606   $aDrag (Aerodynamics)
606   $aLift (Aerodynamics)
606   $aDelta wing airplanes$2fast
606   $aDrag (Aerodynamics)$2fast
606   $aLift (Aerodynamics)$2fast
606   $aVortex flaps$2fast
615  0$aDelta wing airplanes.
615  0$aVortex flaps.
615  0$aDrag (Aerodynamics)
615  0$aLift (Aerodynamics)
615  7$aDelta wing airplanes.
615  7$aDrag (Aerodynamics)
615  7$aLift (Aerodynamics)
615  7$aVortex flaps.
700   $aPolhamus$b Edward C$g(Edward Charles),$f1923-2001,$01417977
712 02$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$bOCLCQ
801  2$bOCLCO
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910715018403321
996   $aApplication of the leading-edge-suction analogy of vortex lift to the drag due to lift of sharp-edge delta wings$93527967
997   $aUNINA