01718oam 2200481I 450 991070651160332120171229140112.0(CKB)5470000002457335(OCoLC)1015374748(OCoLC)995470000002457335(EXLCZ)99547000000245733520171215j201711 ua 0engurmn|||||||||txtrdacontentcrdamediacrrdacarrierDevelopment of an axisymmetric afterbody test case for turbulent flow separation validation /Kevin J. Disotell and Christopher L. RumseyHampton, VA :National Aeronautics and Space Administration, Langley Research Center,November 2017.1 online resource (iv, 27 pages) color illustrationsNASA/TM ;2017-219680"November 2017."Includes bibliographical references (pages 26-27).Turbulence modelsnasatComputational fluid dynamicsnasatAfterbodiesnasatBoundary layer separationnasatSeparated flownasatTurbulence models.Computational fluid dynamics.Afterbodies.Boundary layer separation.Separated flow.Disotell Kevin J.1410943Rumsey C. L(Christopher Lockwood),1961-Langley Research Center,GPOGPOGPOBOOK9910706511603321Development of an axisymmetric afterbody test case for turbulent flow separation validation3500914UNINA