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035   $a(EXLCZ)995470000002522642
100   $a19910305j197210    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 to prediction of longitudinal load distribution and pitching moments for sharp-edged delta wings /$fby Melvin H. Snyder, Jr., and John E. Lamar
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dOctober 1972.
215   $a1 online resource (20 pages) $cillustrations
225 1 $aNASA/TN ;$vD-6994
300   $a"October 1972."
320   $aIncludes bibliographical references (pages 10-11).
606   $aAerodynamic loads$2nasat
606   $aDelta wings$2nasat
606   $aPitching (Aerodynamics)
606   $aAirplanes$xWings, Triangular
606   $aVortex-motion
606   $aAerodynamic load$2fast
606   $aAirplanes$xWings, Triangular$2fast
606   $aPitching (Aerodynamics)$2fast
606   $aVortex-motion$2fast
615  7$aAerodynamic loads.
615  7$aDelta wings.
615  0$aPitching (Aerodynamics)
615  0$aAirplanes$xWings, Triangular.
615  0$aVortex-motion.
615  7$aAerodynamic load.
615  7$aAirplanes$xWings, Triangular.
615  7$aPitching (Aerodynamics)
615  7$aVortex-motion.
700   $aSnyder$b Melvin H.$cJr,$f1921-$01395388
702   $aLamar$b John E.
712 02$aUnited States.$bNational Aeronautics and Space Administration,
712 02$aLangley Research Center.
801  0$bABC
801  1$bABC
801  2$bAD#
801  2$bOCLCE
801  2$bOCLCQ
801  2$bOCLCO
801  2$bOCLCF
801  2$bOCLCQ
801  2$bCOP
801  2$bGPO
906   $aBOOK
912   $a9910716551403321
996   $aApplication of the leading-edge-suction analogy to prediction of longitudinal load distribution and pitching moments for sharp-edged delta wings$93453827
997   $aUNINA