01986oam 2200565 a 450 991070178890332120120820120704.0(CKB)5470000002420205(OCoLC)785219635(EXLCZ)99547000000242020520120410d1985 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierAn airfoil flutter model suspension system to accommodate large static transonic airloads[electronic resource] /Wilmer H. Reed, IIINewport News, VA :DEI-Tech, Inc. ;Hampton, Va. :National Aeronautics and Space Administration, Langley Research Center,[1985]1 online resource (36 pages) illustrationsNASA contractor report ;177998NASA-CR-177998Title from title screen (viewed Apr. 10, 2012)."October 1985."Includes bibliographical references (pages 18-19).AirfoilsnasatBlowdown wind tunnelsnasatFlutter analysisnasatPressure distributionnasatStatic pressurenasatSupercritical airfoilsnasatTransonic wind tunnelsnasatTwo dimensional flownasatAirfoils.Blowdown wind tunnels.Flutter analysis.Pressure distribution.Static pressure.Supercritical airfoils.Transonic wind tunnels.Two dimensional flow.Reed Wilmer H1390193DEI-Tech, Inc.Langley Research Center.GPOGPOGPOBOOK9910701788903321An airfoil flutter model suspension system to accommodate large static transonic airloads3442728UNINA