LEADER 01712nam  2200505   450 
001 9910707158803321
005 20160428074654.0
035   $a(CKB)5470000002461909
035   $a(OCoLC)948163735
035   $a(EXLCZ)995470000002461909
100   $a20160428d1996      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 00$aFinal report for NASA Ames cooperative agreement, NCC2-5049
210  1$a[Davis, Calif.] :$cDepartment of Mechanical and Aeronautical Engineering, University of California, Davis,$d1996.
215   $a1 online resource (7 pages) $cillustrations
225 1 $a[NASA contractor report] ;$vNASA-CR-202567
300   $aTitle from title screen (viewed Apr. 28, 2016).
300   $a"July 1996."
320   $aIncludes bibliographical references.
517 1 $aOptimum shape design using automatic differentiation in reverse mode
606   $aConvergence
606   $aMathematical optimization
606   $aConvergence$2nasat
606   $aSupersonic flow$2nasat
606   $aTransonic flow$2nasat
606   $aOptimization$2nasat
606   $aDesign analysis$2nasat
615  0$aConvergence.
615  0$aMathematical optimization.
615  7$aConvergence.
615  7$aSupersonic flow.
615  7$aTransonic flow.
615  7$aOptimization.
615  7$aDesign analysis.
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910707158803321
996   $aFinal report for NASA Ames cooperative agreement, NCC2-5049$93260302
997   $aUNINA