LEADER 01718oam  2200481I  450 
001 9910706511603321
005 20171229140112.0
035   $a(CKB)5470000002457335
035   $a(OCoLC)1015374748
035   $a(OCoLC)995470000002457335
035   $a(EXLCZ)995470000002457335
100   $a20171215j201711    ua             0
101 0 $aeng
135   $aurmn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aDevelopment of an axisymmetric afterbody test case for turbulent flow separation validation /$fKevin J. Disotell and Christopher L. Rumsey
210  1$aHampton, VA :$cNational Aeronautics and Space Administration, Langley Research Center,$dNovember 2017.
215   $a1 online resource (iv, 27 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2017-219680
300   $a"November 2017."
320   $aIncludes bibliographical references (pages 26-27).
606   $aTurbulence models$2nasat
606   $aComputational fluid dynamics$2nasat
606   $aAfterbodies$2nasat
606   $aBoundary layer separation$2nasat
606   $aSeparated flow$2nasat
615  7$aTurbulence models.
615  7$aComputational fluid dynamics.
615  7$aAfterbodies.
615  7$aBoundary layer separation.
615  7$aSeparated flow.
700   $aDisotell$b Kevin J.$01410943
702   $aRumsey$b C. L$g(Christopher Lockwood),$f1961-
712 02$aLangley Research Center,
801  0$bGPO
801  1$bGPO
801  2$bGPO
906   $aBOOK
912   $a9910706511603321
996   $aDevelopment of an axisymmetric afterbody test case for turbulent flow separation validation$93500914
997   $aUNINA