02491oam 2200649 450 991070747200332120160816141332.0(CKB)5470000002464806(OCoLC)785232000(EXLCZ)99547000000246480620120408j198010 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierCalculation of three-dimensional unsteady transonic flows past helicopter blades /J.J. Chattot[Washington, D.C.] :National Aeronautics and Space Administration, Scientific and Technical Information Branch,October 1980.1 online resource (29 pages) illustrationsNASA technical paper ;1721AVRADCOM technical report ;80-A-2Title from title screen (viewed on Aug. 16, 2016)."October 1980.""Performing Organization: NASA Ames Research Center and Aeromechanics Laboratory AVRADCOM Research and Technology Laboratories"--Report documentation page.Includes bibliographical references (page 19).Difference equationsnasatFinite difference theorynasatHelicopter designnasatRotor aerodynamicsnasatTransonic flownasatHelicoptersAerodynamicsfastRotors (Helicopters)AerodynamicsfastUnsteady flow (Aerodynamics)fastDifference equations.Finite difference theory.Helicopter design.Rotor aerodynamics.Transonic flow.HelicoptersAerodynamics.Rotors (Helicopters)Aerodynamics.Unsteady flow (Aerodynamics)Chattot J. J.965094Ames Research Center.Aeromechanics Laboratory.United States.Army Aviation Research and Development Command.United States.National Aeronautics and Space Administration.Scientific and Technical Information Branch,OCLCEOCLCEOCLCQOCLCOOCLCFOCLCQGPOBOOK9910707472003321Calculation of three-dimensional unsteady transonic flows past helicopter blades3487782UNINA