MARC Record from marc_columbia

LEADER: 04113cam a2200793 i 4500
001 11608404
005 20220604224407.0
006 m o d f
007 cr |||||||||||
008 150724s1957 dcua obt f000 0 eng d
035 $a(OCoLC)ocn914329651
035 $a(NNC)11608404
040 $aSINTU$beng$epn$cSINTU$dKNOVL$dZCU$dTJC$dOCLCQ$dUAB$dREB$dDKU$dOCLCQ$dCEF$dRRP$dYOU$dCOO$dOCLCF$dWYU$dS2H$dOCLCO$dOCLCQ$dOCLCO
019 $a951669598$a987009913
020 $a9781680156300$q(electronic bk.)
020 $a1680156306$q(electronic bk.)
035 $a(OCoLC)914329651$z(OCoLC)951669598$z(OCoLC)987009913
050 4 $aTA645
082 04 $a623.817$223
049 $aZCUA
100 1 $aGerard, George.
245 10 $aHandbook of structural stability.$nPart 5,$pCompressive strength of flat stiffened panels /$cGeorge Gerard.
260 $aWashington, D.C. :$bNational Advisory Committee for Aeronautics,$c[1957]
300 $a1 online resource (ii, 89 pages) :$billustrations
336 $atext$btxt$2rdacontent
337 $acomputer$bc$2rdamedia
338 $aonline resource$bcr$2rdacarrier
490 1 $aTechnical note / National Advisory Committee for Aeronautics ;$v3785
500 $aNACA TN No. 3785.
504 $aIncludes bibliographical references.
520 3 $aA generalized crippling analysis for short monolithic panels with formed or extruded stiffeners is presented. The analysis applies to monolithic panels. Criteria are given for rivete panels which indicate if the panels can be considered to behave in a monolithic manner. Riveted panels that are subject to interrivet buckling and wrinkling or forced crippling do not behave in this manner. Methods are presented for estimating the strength of such panels.
520 3 $aIntermediate-length and long stiffened panels are subject to other failure modes. Methods are given for estimating the column strength of panels. Various forms of column curves and direct-reading charts are considered. Theory and test data on optimum stiffened panels are presented for use in preliminary design studies.
520 3 $aIn box types of construction, the rib and spar structures influence the compressive strength of the stiffened panel. The various factors which can be of importance are considered.
588 0 $aPrint version record.
650 0 $aStructural analysis (Engineering)
650 0 $aStability.
650 0 $aPlates (Engineering)
650 0 $aMaterials$xCompression testing.
650 0 $aBuckling (Mechanics)
650 0 $aLoads (Mechanics)
650 0 $aStrains and stresses.
650 6 $aThéorie des constructions.
650 6 $aStabilité.
650 6 $aPlaques (Ingénierie)
650 6 $aEssais de compression.
650 6 $aFlambage (Résistance des matériaux)
650 6 $aCharges.
650 6 $aContraintes (Mécanique)
650 7 $astructural analysis.$2aat
650 7 $astability.$2aat
650 7 $awarping.$2aat
650 7 $abuckling.$2aat
650 7 $astrain.$2aat
650 7 $astress.$2aat
650 7 $aBuckling (Mechanics)$2fast$0(OCoLC)fst00840001
650 7 $aLoads (Mechanics)$2fast$0(OCoLC)fst01739107
650 7 $aMaterials$xCompression testing.$2fast$0(OCoLC)fst01011785
650 7 $aPlates (Engineering)$2fast$0(OCoLC)fst01066785
650 7 $aStability.$2fast$0(OCoLC)fst01131203
650 7 $aStrains and stresses.$2fast$0(OCoLC)fst01134288
650 7 $aStructural analysis (Engineering)$2fast$0(OCoLC)fst01135602
655 0 $aElectronic books.
655 4 $aElectronic books.
700 1 $aBecker, Herbert,$d1918-
710 1 $aUnited States.$bNational Advisory Committee for Aeronautics.
776 08 $iPrint version:$aGerard, George.$tHandbook of structural stability.$dWashington, D.C. : National Advisory Committee for Aeronautics, [1957]$w(OCoLC)682901595
830 0 $aTechnical note (United States. National Advisory Committee for Aeronautics) ;$vno. 3785.
856 40 $uhttp://www.columbia.edu/cgi-bin/cul/resolve?clio11608404$zACADEMIC - Aerospace & Radar Technology
852 8 $blweb$hEBOOKS