02288oam 2200637 450 991071407530332120201106090117.0(CKB)5470000002506917(OCoLC)761067530(EXLCZ)99547000000250691720111115j196811 ua 0engur|||||||||||txtrdacontentcrdamediacrrdacarrierAerodynamic characteristics of twin-propeller deflected-slipstream STOL airplane model with boundary-layer control on inverted v-tail /by Richard J. Margason and Garl L. Gentry, JrWashington, D.C. :National Aeronautics and Space Administration,November 1968.1 online resource (179 pages) illustrationsNASA technical note ;NASA TN D-4856"November1968."Includes bibliographical references (page 16).Short take-off and landing aircraftBoundary layer controlPropellers, AerialAirplanesTail surfacesAerodynamicsAerodynamicsfastAirplanesTail surfacesfastBoundary layer controlfastPropellers, AerialfastShort take-off and landing aircraftfastShort take-off and landing aircraft.Boundary layer control.Propellers, Aerial.AirplanesTail surfaces.Aerodynamics.Aerodynamics.AirplanesTail surfaces.Boundary layer control.Propellers, Aerial.Short take-off and landing aircraft.Margason Richard J.1170468Gentry Garl L.United States.National Aeronautics and Space Administration,Langley Research Center.OCLCEOCLCEOCLCQOCLCFOCLCQGPOBOOK9910714075303321Aerodynamic characteristics of twin-propeller deflected-slipstream STOL airplane model with boundary-layer control on inverted v-tail3457121UNINA