MARC Record from marc_columbia

LEADER: 03586cam a2200733 i 4500
001 11608413
005 20220528224337.0
006 m o d f
007 cr |||||||||||
008 150727s1943 dcua obt f000 0 eng d
035 $a(OCoLC)ocn914552880
035 $a(NNC)11608413
040 $aSINTU$beng$epn$cSINTU$dKNOVL$dZCU$dOCLCQ$dUAB$dDKU$dOCLCQ$dCEF$dRRP$dWYU$dYOU$dS2H$dOCLCO$dOCLCQ$dOCLCO
019 $a951667803
020 $a9781680156478$q(electronic bk.)
020 $a1680156470$q(electronic bk.)
035 $a(OCoLC)914552880$z(OCoLC)951667803
050 4 $aTA660.P6
082 04 $a624.17765$223
049 $aZCUA
100 1 $aStowell, Elbridge Z.
245 10 $aCritical stress for an infinitely long flat plate with elastically restrained edges under combined shear and direct stress /$cElbridge Z. Stowell and Edward B. Schwartz.
246 3 $aNACA Wartime Reports. Series L.
260 $aWashington, D.C. :$bNational Advisory Committee for Aeronautics,$c[1943]
300 $a1 online resource (16, [3] pages) :$billustrations
336 $atext$btxt$2rdacontent
337 $acomputer$bc$2rdamedia
338 $aonline resource$bcr$2rdacarrier
490 1 $aWartime Report / National Advisory Committee for Aeronautics ;$vno. L340
500 $aNACA Wartime Report L-340.
500 $aOriginally issued as NACA as Advance Restricted Report L3K13 (November 1943).
500 $aPrepared at the Langley Memorial Aeronautical Laboratory, Langley Field, Virginia.
504 $aIncludes bibliographical references.
520 3 $aA simple interaction curve is presented for evaluating the conditions of combined shear and direct stress under which an infinitely long, flat plate with equal elastic restraints against rotation along the edges will become unstable. The theoretical work that led to the interaction curve is presented in the form of appendixes.
588 0 $aPrint version record.
650 0 $aPlates (Engineering)
650 0 $aShear (Mechanics)
650 0 $aBuckling (Mechanics)
650 0 $aLoads (Mechanics)
650 0 $aStrains and stresses.
650 0 $aCharts, diagrams, etc.
650 6 $aPlaques (Ingénierie)
650 6 $aCisaillement (Mécanique)
650 6 $aFlambage (Résistance des matériaux)
650 6 $aCharges.
650 6 $aContraintes (Mécanique)
650 6 $aTableaux, graphiques, etc.
650 7 $ashear stress.$2aat
650 7 $adiagrams.$2aat
650 7 $aBuckling (Mechanics)$2fast$0(OCoLC)fst00840001
650 7 $aCharts, diagrams, etc.$2fast$0(OCoLC)fst00852545
650 7 $aLoads (Mechanics)$2fast$0(OCoLC)fst01739107
650 7 $aPlates (Engineering)$2fast$0(OCoLC)fst01066785
650 7 $aShear (Mechanics)$2fast$0(OCoLC)fst01115422
650 7 $aStrains and stresses.$2fast$0(OCoLC)fst01134288
655 0 $aElectronic books.
655 4 $aElectronic books.
700 1 $aSchwartz, Edward B.
710 1 $aUnited States.$bNational Advisory Committee for Aeronautics.
710 2 $aLangley Aeronautical Laboratory.
776 08 $iPrint version:$aStowell, Elbridge Z.$tCritical stress for an infinitely long flat plate with elastically restrained edges under combined shear and direct stress.$dWashington, D.C. : National Advisory Committee for Aeronautics, [1943]$w(OCoLC)707629297
830 0 $aWartime Reports (United States. National Advisory Committee for Aeronautics) ;$vno. L340.
856 40 $uhttp://www.columbia.edu/cgi-bin/cul/resolve?clio11608413$zACADEMIC - Aerospace & Radar Technology
852 8 $blweb$hEBOOKS