MARC Record from marc_columbia

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001 7514686
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006 m o d
007 cr cn|||||||||
008 091111s2006 vaua ob 001 0 eng d
010 $z 2007531073
035 $a(OCoLC)ocn465027503
035 $a(NNC)7514686
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020 $a9781615830756$q(electronic bk.)
020 $a1615830758$q(electronic bk.)
020 $a9781600864636$q(e-book)
020 $a1600864635$q(e-book)
020 $z1563478323
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020 $z9781563476975
020 $a9781600866821
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037 $bKnovel Corporation$nhttp://www.knovel.com
042 $adlr
050 4 $aTA664$b.H64 2006eb
082 04 $a624.1821$222
049 $aZCUA
100 1 $aHodges, Dewey H.
245 10 $aNonlinear composite beam theory /$cDewey H. Hodges.
260 $aReston, Va. :$bAmerican Institute of Aeronautics and Astronautics,$c©2006.
300 $a1 online resource (xii, 304 pages) :$billustrations
336 $atext$btxt$2rdacontent
337 $acomputer$bc$2rdamedia
338 $aonline resource$bcr$2rdacarrier
347 $adata file$2rda
490 1 $aProgress in astronautics and aeronautics ;$vv. 213
504 $aIncludes bibliographical references (pages 291-300) and index.
588 0 $aPrint version record.
506 $3Use copy$fRestrictions unspecified$2star$5MiAaHDL
533 $aElectronic reproduction.$b[Place of publication not identified] :$cHathiTrust Digital Library,$d2011.$5MiAaHDL
538 $aMaster and use copy. Digital master created according to Benchmark for Faithful Digital Reproductions of Monographs and Serials, Version 1. Digital Library Federation, December 2002.$uhttp://purl.oclc.org/DLF/benchrepro0212$5MiAaHDL
583 1 $adigitized$c2011$hHathiTrust Digital Library$lcommitted to preserve$2pda$5MiAaHDL
506 $aAccess restricted to Ryerson students, faculty and staff.$5CaOTR
520 $aBeginning with an overview of the theory developed over the last 60 years, Dr. Hodges addresses the kinematics of beam deformation, provides a simple way to characterize strain in an initially curved and twisted beam, and offers cross-sectional analysis for beams with arbitrary cross sections and composed of arbitrary materials. He goes on to present a way to accurately recover all components of cross-sectional strain and stress before providing a natural one-dimensional (1-D) theory of beams. Sample results for both cross-sectional and 1-D analysis are presented as is a parallel treatment for thin-walled beams.
505 0 $aIntroduction -- Kinematical Preliminaries -- Kinematics of Beams -- Cross-Sectional Analysis for Beams -- One-Dimensional Theory of Beams -- Thin-Walled Beams -- Validation and Sample Results -- A Look Back and a Look Forward -- Appendix A: VABS Tutorial -- Appendix B: Finding Lagrange Multipliers for Mixed Method -- Appendix C: Variables for Nonlinear Theory of Strips.
650 0 $aComposite construction.
650 0 $aGirders$xMathematical models.
650 0 $aGirders.
650 6 $aPoutres.
650 6 $aConstruction mixte.
650 6 $aPoutres$xModèles mathématiques.
650 7 $acomposite construction.$2aat
650 7 $aGirders.$2fast$0(OCoLC)fst00942818
650 7 $aComposite construction.$2fast$0(OCoLC)fst00871671
650 7 $aGirders$xMathematical models.$2fast$0(OCoLC)fst00942830
650 7 $aVerbundwerkstoff$2gnd
650 7 $aNichtlineare Berechnung$2gnd
650 7 $aNichtlineare Mechanik$2gnd
650 7 $aBalken$2gnd
655 0 $aElectronic book.
655 4 $aElectronic books.
776 08 $iPrint version:$aHodges, Dewey H.$tNonlinear composite beam theory.$dReston, Va. : American Institute of Aeronautics and Astronautics, ©2006$z1563478323$w(DLC) 2007531073$w(OCoLC)67520797
830 0 $aProgress in astronautics and aeronautics ;$vv. 213.
856 40 $uhttp://www.columbia.edu/cgi-bin/cul/resolve?clio7514686$zACADEMIC - Aerospace & Radar Technology
852 8 $blweb$hEBOOKS