MARC Record from marc_columbia

LEADER: 03654cam a2200805 i 4500
001 11608460
005 20221203224052.0
006 m o d
007 cr cnu---unuuu
008 150825s1942 dcua obt f000 0 eng d
035 $a(OCoLC)ocn919163322
035 $a(NNC)11608460
040 $aKNOVL$beng$erda$epn$cKNOVL$dZCU$dOCLCQ$dUAB$dDKU$dOCLCQ$dCEF$dRRP$dYOU$dS2H$dOCLCO$dOCLCQ$dUPM
020 $a9781680156539$q(electronic bk.)
020 $a1680156535$q(electronic bk.)
035 $a(OCoLC)919163322
050 4 $aTA480.A6
082 04 $a620.186$223
086 0 $aY 3.N 21/5:11/L402
088 $aNACA WR 402
049 $aZCUA
100 1 $aKuhn, Paul,$eauthor.
245 14 $aThe strength and stiffness of shear webs with and without lightening holes /$cPaul Kuhn.
246 3 $aNACA Wartime Reports. Series L.
264 1 $aWashington, D.C. :$bNational Advisory Committee for Aeronautics,$c[1942]
300 $a1 online resource (29 pages, 15 unnumbered pages) :$billustrations
336 $atext$btxt$2rdacontent
337 $acomputer$bc$2rdamedia
338 $aonline resource$bcr$2rdacarrier
490 1 $aWartime Report / National Advisory Committee for Aeronautics ;$vnumber L402
500 $aNACA Wartime Report L-402.
500 $aOriginally issued as NACA as an Advance Restricted Report (June 1942).
500 $aPrepared at the Langley Memorial Aeronautical Laboratory, Langley Field, Virginia.
504 $aIncludes bibliographical references.
520 3 $aNearly 200 tests were made on the strength of shear webs of 24S-T aluminum alloy, with and without lightening holes. The tests were made in a jig of the single-specimen type, in which the specimen is free to collapse completely without developing diagonal tension. The lightening holes were circular and had either flanged edges or beaded edges, the specimens with flanged edges constituting by far the largest test group.
588 0 $aPrint version record.
650 0 $aAluminum alloys.
650 0 $aHoles.
650 0 $aShear (Mechanics)
650 0 $aStrength of materials.
650 0 $aStrains and stresses.
650 0 $aMonocoque construction.
650 0 $aCharts, diagrams, etc.
650 6 $aAluminium$xAlliages.
650 6 $aTrous.
650 6 $aCisaillement (Mécanique)
650 6 $aRésistance des matériaux.
650 6 $aContraintes (Mécanique)
650 6 $aTableaux, graphiques, etc.
650 7 $aaluminum alloy.$2aat
650 7 $ashear stress.$2aat
650 7 $astrength of materials.$2aat
650 7 $astress.$2aat
650 7 $astrain.$2aat
650 7 $adiagrams.$2aat
650 7 $aAluminum alloys.$2fast$0(OCoLC)fst00806309
650 7 $aCharts, diagrams, etc.$2fast$0(OCoLC)fst00852545
650 7 $aHoles.$2fast$0(OCoLC)fst00958715
650 7 $aMonocoque construction.$2fast$0(OCoLC)fst01025557
650 7 $aShear (Mechanics)$2fast$0(OCoLC)fst01115422
650 7 $aStrains and stresses.$2fast$0(OCoLC)fst01134288
650 7 $aStrength of materials.$2fast$0(OCoLC)fst01134837
655 0 $aElectronic books.
655 4 $aElectronic books.
710 1 $aUnited States.$bNational Advisory Committee for Aeronautics.
710 2 $aLangley Aeronautical Laboratory.
776 08 $iPrint version:$aKuhn, Paul.$tStrength and stiffness of shear webs with and without lightening holes$w(OCoLC)707923695
830 0 $aWartime Reports (United States. National Advisory Committee for Aeronautics) ;$vno. L402.
856 40 $uhttp://www.columbia.edu/cgi-bin/cul/resolve?clio11608460$zACADEMIC - Aerospace & Radar Technology
852 8 $blweb$hEBOOKS