02299oam 2200577 450 991070402480332120151103115242.0(CKB)5470000002437409(OCoLC)761470267(EXLCZ)99547000000243740920111115j198308 ua 0engurbn||||a|a||txtrdacontentcrdamediacrrdacarrierAeromechanical stability of a hingeless rotor in hover and forward flight analysis and wind tunnel tests /William T. Yeager, Jr., M-Nabil H. Hamouda, Wayne R. MantayHampton, Virginia :National Aeronautics and Space Administration, Langley Research Center,August 1983.1 online resource (19 pages) illustrationsNASA technical memorandum ;85683AVRADCOM technical report ;83-B-5Title from title screen (viewed Nov. 3, 2015)."August 1983.""Performing organization: Structures Laboratory, AVRADCOM Research and Technology Laboratories, NASA Langley Research Center"--Technical report page.Includes bibliographical references (pages 9-10).Aeromechanical stability of a hingeless rotor in hover and forward flight Rigid rotorsnasatRotor aerodynamicsnasatGround resonancenasatHorizontal flightnasatHoveringnasatRigid rotors.Rotor aerodynamics.Ground resonance.Horizontal flight.Hovering.Yeager William T.1398153Hamouda M-Nabil H.Mantay Wayne R.Army Research and Technology Laboratories (U.S.).Structures Laboratory,Langley Research Center,United States.National Aeronautics and Space Administration,United States.Army Aviation Research and Development Command,OCLCEOCLCEOCLCQGPOBOOK9910704024803321Aeromechanical stability of a hingeless rotor in hover and forward flight3460942UNINA