01991nam 2200529I 450 991070711610332120160601155159.0(CKB)5470000002462340(OCoLC)950980762(EXLCZ)99547000000246234020160601j201601 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierComparison of NACA 0012 laminar flow solutions: structured and unstructured grid methods /R.C. Swanson, S. Langer[Hampton, VA] :National Aeronautics and Space Administration, Langley Research Center,January 2016.1 online resource (56 pages) color illustrationsNASA/TM ;2016-219003Title from title screen (viewed on June 1, 2016)."January 2016.""Performing organization: NASA Langley Research Center, Hampton, VA"--Report documentation page.Includes bibliographical references (pages 25-27).Comparison of NACA 0012 laminar flow solutionsCompressible flownasatComputational fluid dynamicsnasatComputational geometrynasatLaminar flownasatNavier-Stokes equationnasatSteady statenasatCompressible flow.Computational fluid dynamics.Computational geometry.Laminar flow.Navier-Stokes equation.Steady state.Swanson R. Charles1401804Langer S.Langley Research Center,United States.National Aeronautics and Space Administration,GPOGPOBOOK9910707116103321Comparison of NACA 0012 laminar flow solutions: structured and unstructured grid methods3477237UNINA