02284oam 2200661 450 991071655140332120210623121419.0(CKB)5470000002522642(OCoLC)23191302(OCoLC)761200313(OCoLC)785204937(EXLCZ)99547000000252264219910305j197210 ua 0engur|||||||||||txtrdacontentcrdamediacrrdacarrierApplication of the leading-edge-suction analogy to prediction of longitudinal load distribution and pitching moments for sharp-edged delta wings /by Melvin H. Snyder, Jr., and John E. LamarWashington, D.C. :National Aeronautics and Space Administration,October 1972.1 online resource (20 pages) illustrationsNASA/TN ;D-6994"October 1972."Includes bibliographical references (pages 10-11).Aerodynamic loadsnasatDelta wingsnasatPitching (Aerodynamics)AirplanesWings, TriangularVortex-motionAerodynamic loadfastAirplanesWings, TriangularfastPitching (Aerodynamics)fastVortex-motionfastAerodynamic loads.Delta wings.Pitching (Aerodynamics)AirplanesWings, Triangular.Vortex-motion.Aerodynamic load.AirplanesWings, Triangular.Pitching (Aerodynamics)Vortex-motion.Snyder Melvin H.Jr,1921-1395388Lamar John E.United States.National Aeronautics and Space Administration,Langley Research Center.ABCABCAD#OCLCEOCLCQOCLCOOCLCFOCLCQCOPGPOBOOK9910716551403321Application of the leading-edge-suction analogy to prediction of longitudinal load distribution and pitching moments for sharp-edged delta wings3453827UNINA