02008oam 2200601 450 991071501840332120201130132459.0(CKB)5470000002507823(OCoLC)761173274(EXLCZ)99547000000250782320111115j196808 ua 0engur|||||||||||txtrdacontentcrdamediacrrdacarrierApplication of the leading-edge-suction analogy of vortex lift to the drag due to lift of sharp-edge delta wings /by Edward C. PolhamusWashington, D.C. :National Aeronautics and Space Administration,August 1968.1 online resource (14 pages) illustrationsNASA technical note ;TN D-4739"August 1968."Includes bibliographical references (page 8).Delta wing airplanesVortex flapsDrag (Aerodynamics)Lift (Aerodynamics)Delta wing airplanesfastDrag (Aerodynamics)fastLift (Aerodynamics)fastVortex flapsfastDelta wing airplanes.Vortex flaps.Drag (Aerodynamics)Lift (Aerodynamics)Delta wing airplanes.Drag (Aerodynamics)Lift (Aerodynamics)Vortex flaps.Polhamus Edward C(Edward Charles),1923-2001,1417977United States.National Aeronautics and Space Administration,Langley Research Center.OCLCEOCLCEOCLCQOCLCFOCLCQOCLCOOCLCQGPOBOOK9910715018403321Application of the leading-edge-suction analogy of vortex lift to the drag due to lift of sharp-edge delta wings3527967UNINA