| Record ID | bcl_marc/bcl_open.03.mrc:201311845:1390 |
| Source | bcl_marc |
| Download Link | /show-records/bcl_marc/bcl_open.03.mrc:201311845:1390?format=raw |
LEADER: 01390nam 22003497a 4500
004 GPP4141
005 20000524102300.0
008 990119s1995 dcu b f000 0 eng d
035 $a(OCoLC)ocm40642288
035 9 $aGPP4141
037 $a19970010645$bNASA
040 $aGPO$cGPO$dDLC$dMvI
049 $aBXMX
074 $a0830-H-14 (MF)
086 0 $aNAS 1.26:203261
100 1 $aFeng, Dan.
245 10 $aAerodynamic design optimization via reduced Hessian SQP with solution refining$h[microform] /$cDan Feng and Thomas H. Pulliam.
260 $a[Washington, DC] :$bResearch Institute for Advanced Computer Science, NASA Ames Research Center ;$a[Springfield, Va. :$bNational Technical Information Service, distributor,$c1995]
300 $a1 v.
440 0 $aNASA contractor report ;$vNASA CR-203261
490 1 $aRIACS technical report ;$v95-24
500 $aShipping list no.: 98-1104-M.
533 $aMicrofiche.$b[Washington, D.C. :$cNational Aeronautics and Space Administration,$d1997]$e1 microfiche.
650 7 $aAerodynamics.$2nasat
650 7 $aOptimization.$2nasat
650 7 $aNozzle design.$2nasat
650 7 $aDesign analysis.$2nasat
700 1 $aPulliam, Thomas H.
710 2 $aResearch Institute for Advanced Computer Science (U.S.)
830 0 $aRIACS technical report$vTR-95-24.
852 30 $aMChB$bGOV$cFICHE$hNAS 1.26:203261$91
948 $aLTI 08/08/2000