| Record ID | marc_loc_2016/BooksAll.2016.part06.utf8:134139570:1153 |
| Source | Library of Congress |
| Download Link | /show-records/marc_loc_2016/BooksAll.2016.part06.utf8:134139570:1153?format=raw |
LEADER: 01153cam a22002891 4500
001 68001221
003 DLC
005 19900221104542.9
008 700608s1967 caua b 00010 eng
010 $a 68001221 //r90
040 $aDLC$cDLC$dDLC
050 00 $aTA660.P6$bM37
082 00 $a620.1/1282
100 10 $aMartin, Harold Clifford,$d1913-
245 10 $aStiffness matrix for a triangular sandwich element in bending$c[by] H. C. Martin.
260 0 $aPasadena,$bJet Propulsion Laboratory, California Institute of Technology,$c1967.
300 $aviii, 23 p.$billus.$c28 cm.
490 1 $aJPL technical report 32-1158
500 $a"Prepared under contract no. NAS 7-100, National Aeronautics & Space Administration."
504 $aBibliography: p. 22-23.
650 0 $aPlates (Engineering)
650 0 $aShells (Engineering)
650 0 $aStructural analysis (Engineering)$xMatrix methods.
650 0 $aFlexure.
650 0 $aSandwich construction.
710 10 $aUnited States.$bNational Aeronautics and Space Administration.
810 2 $aCalifornia Institute of Technology, Pasadena.$bJet Propulsion Laboratory.$tJPL technical report$vno. 32-1158