MARC Record from marc_columbia

LEADER: 03815cam a2200769 a 4500
001 11608419
005 20220625224424.0
006 m o d f
007 cr |||||||||||
008 150728s1945 dcua obt f000 0 eng d
035 $a(OCoLC)ocn914578705
035 $a(NNC)11608419
040 $aSINTU$beng$epn$cSINTU$dKNOVL$dZCU$dOCLCQ$dUAB$dCOD$dMERER$dOCLCQ$dOCLCF$dDKU$dOCLCQ$dCEF$dRRP$dYOU$dS2H$dOCLCO$dOCLCQ$dOCLCO
019 $a951674112
020 $a9781680156393$q(electronic bk.)
020 $a168015639X$q(electronic bk.)
035 $a(OCoLC)914578705$z(OCoLC)951674112
050 4 $aTA480.A6
082 04 $a620.186$223
049 $aZCUA
100 1 $aLundquist, Eugene E.
245 10 $aPrinciples of moment distribution applied to stability of structures composed of bars or plates /$cEugene E. Lundquist, Elbridge Z. Stowell, and Evan H. Schuette.
260 $aWashington, D.C. :$bU.S. Government Printing Office,$c1948.
300 $a1 online resource (14 pages) :$billustrations
336 $atext$btxt$2rdacontent
337 $acomputer$bc$2rdamedia
338 $aonline resource$bcr$2rdacarrier
490 1 $aReport / National Advisory Committee for Aeronautics ;$vno. 809
500 $aPrepared at the Langley Memorial Aeronautical Laboratory, Langley Field, Virginia.
504 $aIncludes bibliographical references.
520 3 $aThe principles of the cross method of moment distribution, which have previously been applied to the stability of structures composed of bars under axial load, are applied to the stability of structures composed of long plates under longitudinal load. A brief theoretical treatment of the subject, as applied to structures composed of either bars or plates, is included, together with an illustrative example for each of these two types of structure. An appendix presents the derivation of the formulas for the various stiffnesses and carry-over factors used in solving problems in the stability of structures composed of long plates.
588 0 $aPrint version record.
650 0 $aAluminum alloys.
650 0 $aBars (Engineering)
650 0 $aPlates (Engineering)
650 0 $aBuckling (Mechanics)
650 0 $aStrains and stresses.
650 0 $aStability.
650 6 $aAluminium$xAlliages.
650 6 $aBarres (Ingénierie)
650 6 $aPlaques (Ingénierie)
650 6 $aFlambage (Résistance des matériaux)
650 6 $aContraintes (Mécanique)
650 6 $aStabilité.
650 7 $aaluminum alloy.$2aat
650 7 $abars (building materials)$2aat
650 7 $awarping.$2aat
650 7 $abuckling.$2aat
650 7 $astress.$2aat
650 7 $astrain.$2aat
650 7 $astability.$2aat
650 7 $aAluminum alloys.$2fast$0(OCoLC)fst00806309
650 7 $aBars (Engineering)$2fast$0(OCoLC)fst00827804
650 7 $aBuckling (Mechanics)$2fast$0(OCoLC)fst00840001
650 7 $aPlates (Engineering)$2fast$0(OCoLC)fst01066785
650 7 $aStability.$2fast$0(OCoLC)fst01131203
650 7 $aStrains and stresses.$2fast$0(OCoLC)fst01134288
655 0 $aElectronic books.
655 4 $aElectronic books.
700 1 $aStowell, Elbridge Z.
700 1 $aSchuette, Evan H.
710 1 $aUnited States.$bNational Advisory Committee for Aeronautics.
710 2 $aLangley Aeronautical Laboratory.
776 08 $iPrint version:$aLundquist, Eugene E.$tPrinciples of moment distribution applied to stability of structures composed of bars or plates.$dWashington, D.C. : U.S. Government Printing Office, 1948$w(OCoLC)893499384
830 0 $aReport (United States. National Advisory Committee for Aeronautics) ;?v no. 809.
856 40 $uhttp://www.columbia.edu/cgi-bin/cul/resolve?clio11608419$zACADEMIC - Aerospace & Radar Technology
852 8 $blweb$hEBOOKS