01858oam 2200529I 450 991070439950332120160223101054.0(CKB)5470000002439685(OCoLC)755284190(EXLCZ)99547000000243968520111002j199608 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierArtificial boundary conditions for computation of oscillating external flows /S.V. TsynkovHampton, Virginia :National Aeronautics and Space Administration, Langley Research Center,August 1996.1 online resource (43 pages) illustrationsNASA technical memorandum ;4714Title from title screen (viewed on Feb. 23, 2016)."August 1996.""Performing organization: NASA Langley Research Center, Hampton, VA"--Report documentation page.Includes bibliographical references (pages 42-43).Boundary conditionsnasatAirfoilsnasatFinite difference theorynasatOscillating flownasatBoundary layersnasatBoundary conditions.Airfoils.Finite difference theory.Oscillating flow.Boundary layers.Tsynkov Semyon V.1399294Langley Research Center,United States.National Aeronautics and Space Administration,OCLCEOCLCEOCLCQOCLCFOCLCOGPOBOOK9910704399503321Artificial boundary conditions for computation of oscillating external flows3464231UNINA