| Record ID | marc_oregon_summit_records/catalog_files/osu_bibs.mrc:930167533:2143 |
| Source | Oregon Libraries |
| Download Link | /show-records/marc_oregon_summit_records/catalog_files/osu_bibs.mrc:930167533:2143?format=raw |
LEADER: 02143nam a22005297a 4500
001 32197785
003 OR
008 950602s1994 vau b f000 0 eng d
035 $a10913166
037 $aN 95-11946$bNASA
040 $aDGPO$cDGPO$dDLC
049 $aORE1$lbna
074 $a0830-H-14 (MF)
086 $aNAS 1.26:196851
086 0 $aNAS 1.26:196851
099 $aNAS 1.26:196851
100 1 $aHarrison, Peter N.
245 10 $aInterlaminar stress analysis of dropped-ply laminated plates and shells by a mixed method$h[microform] /$cPeter N. Harrison, Eric R. Johnson, James H. Starnes.
246 3 $aInterlaminar stress analysis of dropped ply laminated plates and shells by a mixed method.
260 $aBlacksburg, Va. :$bVirginia Polytechnic Institute and State University ;$a[Washington, DC :$bNational Aeronautics and Space Administration ;$aSpringfield, Va. :$bNational Technical Information Service, distributor,$c1994]
300 $a1 v.
440 0 $aNASA contractor report ;$vNASA CR-196851.
533 $aMicrofiche.$b[Washington, D.C. :$cNational Aeronautics and Space Administration,$d1994]$e1 microfiche.
500 $aDistributed to depository libraries in microfiche.
500 $aShipping list no.: 95-0069-M.
650 7 $aAxisymmetric bodies.$2nasat.
650 7 $aBoundary value problems.$2nasat.
650 7 $aCylindrical shells.$2nasat.
650 7 $aFinite difference theory.$2nasat.
650 7 $aInterlaminar stress.$2nasat.
650 7 $aLaminates.$2nasat.
650 7 $aLoads (Forces)$2nasat.
650 7 $aPlates (Structural members)$2nasat.
650 7 $aPly orientation.$2nasat.
650 7 $aReissner theory.$2nasat.
650 7 $aRunge-Kutta method.$2nasat.
650 7 $aStress analysis.$2nasat.
650 7 $aStress distribution.$2nasat.
700 1 $aJohnson, Eric R.
700 1 $aStarnes, James H.
710 1 $aUnited States.$bNational Aeronautics and Space Administration.
907 $a.b18404443$bvdo $c-
902 $a020110
998 $b1$c981001$dm$ea$f-$g0
937 $aAssessment exclusion record.
999 $a19950602110931.0
945 $lvdonf$e1