| Record ID | marc_university_of_toronto/uoft.marc:3687132251:1006 |
| Source | University of Toronto |
| Download Link | /show-records/marc_university_of_toronto/uoft.marc:3687132251:1006?format=raw |
LEADER: 01006cam 22002412a 4500
008 000000s1982 onc m eng d
090 $aTHESIS M 230$bAERO$c2
090 $aTHESIS M 230$bAERO
100 1 $aOstaff, Paul Matthew.
245 14 $aThe buckling of asymmetric composite shells under axial compressive load /$cPaul Matthew Ostaff.
260 $a[Downsview, Ont.] :$bDept. of Aerospace Science and Engineering,$c1982.
300 $a1 v. (various pagings) :$bill.
502 $aThesis (M.A.Sc.) - University of Toronto, 1982.
504 $aIncludes bibliographical references.
650 7 $aAxial compression loads$2nasat
650 7 $aBuckling$2nasat
650 7 $aCylindrical shells$2nasat
650 7 $aGraphite-epoxy composites$2nasat
650 7 $aLaminates$2nasat
948 $a01/08/2001$b03/16/2001
039 $f//ws
949 $aTHESIS M 230$wLC$c1$i34444022745566$lSTACKS$mAEROSPACE$rY$sY$tBOOK$u28/1/2001
949 $aTHESIS M 230$wLC$c2$i34444023059488$lSTACKS$mAEROSPACE$rY$sY$tBOOK$u28/3/2001