01974oam 2200589 450 991071517060332120201211125543.0(CKB)5470000002508306(OCoLC)761497571(EXLCZ)99547000000250830620111115j196808 ua 0engur|||||||||||txtrdacontentcrdamediacrrdacarrierEffect of hinge-line bleed on heat transfer and pressure distribution over a wedge-flap combination at Mach 10.4 /by H. Harris Hamilton, and J. David DearingWashington, D.C. :National Aeronautics and Space Administration,August 1968.1 online resource (44 pages) illustrationsNASA technical note ;TN D-4686"August 1968."Includes bibliographical references (pages 18-21).Boundary layer controlFlaps (Airplanes)WedgesAircraft separationAircraft separationfastBoundary layer controlfastFlaps (Airplanes)fastWedgesfastBoundary layer control.Flaps (Airplanes)Wedges.Aircraft separation.Aircraft separation.Boundary layer control.Flaps (Airplanes)Wedges.Hamilton H. Harris1405571Dearing J. DavidUnited States.National Aeronautics and Space Administration,Langley Research Center.OCLCEOCLCEOCLCQOCLCFOCLCQGPOBOOK9910715170603321Effect of hinge-line bleed on heat transfer and pressure distribution over a wedge-flap combination at Mach 10.43482420UNINA