02021oam 2200541 450 991070780410332120170111112438.0(CKB)5470000002468522(OCoLC)761261209(EXLCZ)99547000000246852220111115j198711 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierIntegration effects of D-shaped, underwing, aft-mounted, separate-flow, flow-through nacelles on a high-wing transport /Milton Lamb, John R. Carlson, and Odis C. PendergraftWashington, D.C. :National Aeronautics and Space Administration, Scientific and Technical Information Division,November 1987.1 online resource (21 pages) illustrationsNASA technical memorandum ;4018"November 1987.""Performing organization: NASA Langley Research Center"--Report documentation page.Includes bibliographical references (page 3).Angle of attacknasatNacellesnasatSeparated flownasatSupersonic flownasatTransonic wind tunnelsnasatAngle of attack.Nacelles.Separated flow.Supersonic flow.Transonic wind tunnels.Lamb Milton1393161Carlson John R.Pendergraft Odis C.Langley Research Center.United States.National Aeronautics and Space Administration.Scientific and Technical Information Division.OCLCEOCLCEOCLCQOCLCOOCLCQGPOBOOK9910707804103321Integration effects of D-shaped, underwing, aft-mounted, separate-flow, flow-through nacelles on a high-wing transport3448935UNINA