01973oam 2200529I 450 991070574930332120170622150731.0(CKB)5470000002452914(OCoLC)990788328(EXLCZ)99547000000245291420170622d1995 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierApplication of a Navier-Stokes solver to the analysis of multielement airfoils and wings using multizonal grid techniques /Kenneth M. Jones, Robert T. Biedron, Mark Whitlock[Washington, D.C.]:National Aeronautics and Space Administration,[1995].1 online resource (25 pages) illustrationsNASA-TM ;112005"13th Applied Aerodynamics Conference June 19-22, 1995, San Diego, California.""AIAA 95-1855."Includes bibliographical references (page 12).Aerodynamic configurationsnasatAirfoilsnasatComputational fluid dynamicsnasatNavier-Stokes equationnasatReynolds numbernasatWing flapsnasatAerodynamic configurations.Airfoils.Computational fluid dynamics.Navier-Stokes equation.Reynolds number.Wing flaps.Jones Kenneth M.1408986Biedron Robert T.Whitlock MarkAmerican Institute of Aeronautics and Astronautics.United States.National Aeronautics and Space Administration,GPOGPOGPOBOOK9910705749303321Application of a Navier-Stokes solver to the analysis of multielement airfoils and wings using multizonal grid techniques3514416UNINA