01964nam 2200505 450 991070795350332120170202145107.0(CKB)5470000002469033(OCoLC)971137366(EXLCZ)99547000000246903320170202j199304 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierExperimental effects of wing location on wing-body pressures at supersonic speeds /Jerry M. Allen and Carolyn B. Watson[Washington, D.C.] :National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program,April 1993.1 online resource (195 pages) illustrationsNASA technical memorandum ;4434"April 1993" Report documentation page."Performing organization: NASA Langley Research Center"--Report documentation page.Includes bibliographical references (page 6).Angle of attacknasatBody-wing configurationsnasatFlow coefficientsnasatPressure distributionnasatSupersonic flightnasatSupersonic speednasatAngle of attack.Body-wing configurations.Flow coefficients.Pressure distribution.Supersonic flight.Supersonic speed.Allen Jerry M.1400290Watson Carolyn B.Langley Research Center.United States.National Aeronautics and Space Administration.Scientific and Technical Information Program,GPOGPOBOOK9910707953503321Experimental effects of wing location on wing-body pressures at supersonic speeds3541323UNINA