LEADER 02008nam  2200481I  450 
001 9910704019103321
005 20151119163650.0
035   $a(CKB)5470000002437467
035   $a(OCoLC)929990245
035   $a(EXLCZ)995470000002437467
100   $a20151119j201508    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 13$aAn automated DAKOTA and VULCAN-CFD framework with application to supersonic facility nozzle flowpath optimization /$fErik L. Axdahl
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dAugust 2015.
215   $a1 online resource (31 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2015-218796
300   $aTitle from title screen (viewed on Nov. 19, 2015).
300   $a"August 2015."
320   $aIncludes bibliographical references (pages 14-15).
517 3 $aAutomated design analysis kit for optimization and terascale applications and viscous upwind algorithm for complex flow analysis computational fluid dynamics framework with application to supersonic facility nozzle flowpath optimization
606   $aComputational fluid dynamics$2nasat
606   $aDesign optimization$2nasat
606   $aSupersonic nozzles$2nasat
606   $aNumerical analysis$2nasat
606   $aTest facilities$2nasat
615  7$aComputational fluid dynamics.
615  7$aDesign optimization.
615  7$aSupersonic nozzles.
615  7$aNumerical analysis.
615  7$aTest facilities.
700   $aAxdahl$b Erik L.$01398384
712 02$aLangley Research Center,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910704019103321
996   $aAn automated DAKOTA and VULCAN-CFD framework with application to supersonic facility nozzle flowpath optimization$93461515
997   $aUNINA