LEADER 01817nam  2200529 a 450 
001 9910700147003321
005 20110321152245.0
035   $a(CKB)5470000002407497
035   $a(OCoLC)707937417
035   $a(EXLCZ)995470000002407497
100   $a20110321d2010      ua             0
101 0 $aeng
135   $aurmn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 00$aMultifidelity analysis and optimization for supersonic design$b[electronic resource] /$fIlan Kroo ... [and others]
210  1$aHampton, Va. :$cNational Aeronautics and Space Administration, Langley Research Center,$d[2010]
215   $a1 online resource (115 pages) $cillustrations
225 1 $aNASA/CR-2010-216874
300   $aTitle from title screen (viewed on March 21, 2011).
300   $a"December 2010."
320   $aIncludes bibliographical references (pages 112-115).
606   $aSupersonic aircraft$2nasat
606   $aAerodynamic characteristics$2nasat
606   $aDesign analysis$2nasat
606   $aDesign to cost$2nasat
606   $aOptimization$2nasat
606   $aPanel method (fluid dynamics)$2nasat
606   $aSupersonic drag$2nasat
606   $aSupersonic airfoils$2nasat
615  7$aSupersonic aircraft.
615  7$aAerodynamic characteristics.
615  7$aDesign analysis.
615  7$aDesign to cost.
615  7$aOptimization.
615  7$aPanel method (fluid dynamics)
615  7$aSupersonic drag.
615  7$aSupersonic airfoils.
701   $aKroo$b Ilan$01396077
712 02$aLangley Research Center.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910700147003321
996   $aMultifidelity analysis and optimization for supersonic design$93455616
997   $aUNINA