| Record ID | marc_oregon_summit_records/catalog_files/washs02192008.mrc_revrev.mrc:1269474409:1663 |
| Source | Oregon Libraries |
| Download Link | /show-records/marc_oregon_summit_records/catalog_files/washs02192008.mrc_revrev.mrc:1269474409:1663?format=raw |
LEADER: 01663nam a2200397Ka 4500
001 37958339
003 OCoLC
005 19980310122125.0
008 971118s1996 dcu b f000 0 eng d
037 $aN 97-13249$bNASA
040 $aGPO$cGPO$dNTE
049 $aNTEI
074 $a0830-D (MF)
086 0 $aNAS 1.15:4770
100 1 $aKo, William L.
245 10 $aThermal and mechanical buckling analysis of hypersonic aircraft hat-stiffened panels with varying face sheet geometry and fiber orientation$h[microform] /$cWilliam L. Ko.
260 $a[Washington, DC] :$bNational Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;$a[Springfield, Va. :$bNational Technical Information Service, distributor],$c1996.
300 $a1 v.
440 0 $aNASA technical memorandum ;$v4770.
500 $aDistributed to depository libraries in microfiche.
500 $aShipping list no.: 97-0960-M.
533 $aMicrofiche.$b[Washington, D.C. :$cNational Aeronautics and Space Administration,$d1997]$e1 microfiche.
650 7 $aAircraft structures.$2nasat.
650 7 $aPanels.$2nasat.
650 7 $aThermal buckling.$2nasat.
650 7 $aMechanical properties.$2nasat.
650 7 $aFinite element method.$2nasat.
650 7 $aHypersonic aircraft.$2nasat.
650 7 $aFiber orientation.$2nasat.
710 1 $aUnited States.$bNational Aeronautics and Space Administration.$bScientific and Technical Information Program.
907 $a.b25192966$bwo $c-
902 $a040717
998 $b1$c980311$dm$ea$f-$g0
907 $a.b25192966
907 $a.b25192966
945 $lwoxau$aNAS 1.15:4770