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MARC Record from marc_columbia

Record ID marc_columbia/Columbia-extract-20221130-024.mrc:62019498:3322
Source marc_columbia
Download Link /show-records/marc_columbia/Columbia-extract-20221130-024.mrc:62019498:3322?format=raw

LEADER: 03322cam a2200709 i 4500
001 11608398
005 20221022224049.0
006 m o d f
007 cr |||||||||||
008 150724s1952 ohua obt f000 0 eng d
035 $a(OCoLC)ocn914328247
035 $a(NNC)11608398
040 $aSINTU$beng$epn$cSINTU$dSINTU$dKNOVL$dZCU$dOCLCQ$dUAB$dDKU$dOCLCQ$dCEF$dRRP$dYOU$dS2H$dOCLCO$dOCLCQ$dOCLCO$dTRAAL
019 $a951660471
020 $a9781680156201$q(electronic bk.)
020 $a1680156209$q(electronic bk.)
035 $a(OCoLC)914328247$z(OCoLC)951660471
050 4 $aTA660.P6
082 04 $a624.17765$223
086 0 $aY 3.N 21/5:6/2661
088 $aNACA-TN-2661
049 $aZCUA
100 1 $aKuhn, Paul.
245 12 $aA summary of diagonal tension.$nPart 1,$pMethods and analysis /$cPaul Kuhn, James P. Peterson, and L. Ross Levin.
260 $aWashington, D.C. :$bNational Advisory Committee for Aeronautics,$c1952.
300 $a1 online resource (131 pages) :$billustrations
336 $atext$btxt$2rdacontent
337 $acomputer$bc$2rdamedia
338 $aonline resource$bcr$2rdacarrier
490 1 $aNational Advisory Committee for Aeronautics ;$vno. 2661
500 $a"May 1952."
500 $aNACA TN No. 2661.
504 $aIncludes bibliographical references.
520 3 $aPreviously published methods for stress and strength analysis of plane and curved shear webs working in diagonal tension are presented as a unified method. The treatment is sufficiently comprehensive and detailed to make the paper self-contained. Part 1 discusses the theory and methods for calculating the stresses and shear deflections of web systems as well as the strengths of the web, the stiffeners, and the riveting. Part 2, published separately, presents the experimental evidence.
588 0 $aPrint version record.
650 0 $aPlates (Engineering)
650 0 $aBars (Engineering)
650 0 $aStrains and stresses.
650 0 $aShear (Mechanics)
650 0 $aMathematical analysis.
650 6 $aPlaques (Ingénierie)
650 6 $aBarres (Ingénierie)
650 6 $aContraintes (Mécanique)
650 6 $aCisaillement (Mécanique)
650 6 $aAnalyse mathématique.
650 7 $abars (building materials)$2aat
650 7 $ashear stress.$2aat
650 7 $aBars (Engineering)$2fast$0(OCoLC)fst00827804
650 7 $aMathematical analysis.$2fast$0(OCoLC)fst01012068
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 $aPeterson, James P.
700 1 $aLevin, L. Ross.
710 1 $aUnited States.$bNational Advisory Committee for Aeronautics.
730 0 $aTechnical Report Archive & Image Library (TRAIL)
776 08 $iPrint version:$aKuhn, Paul.$tSummary of diagonal tension.$dWashington, D.C. : National Advisory Committee for Aeronautics, 1952$w(OCoLC)667213346
830 0 $aTechnical note (United States. National Advisory Committee for Aeronautics) ;$vno. 2661.
856 40 $uhttp://www.columbia.edu/cgi-bin/cul/resolve?clio11608398$zACADEMIC - Aerospace & Radar Technology
852 8 $blweb$hEBOOKS