MARC Record from marc_columbia

LEADER: 02915cam a2200565 i 4500
001 11608457
005 20221203224051.0
006 m o d
007 cr cnu---unuuu
008 150825s1938 dcua ob f000 0 eng d
035 $a(OCoLC)ocn919150706
035 $a(NNC)11608457
040 $aKNOVL$beng$erda$epn$cKNOVL$dOCLCF$dZCU$dUAB$dDKU$dOCLCQ$dCEF$dRRP$dYOU$dS2H$dOCLCO$dOCLCQ$dUPM
020 $a9781680156409$q(electronic bk.)
020 $a1680156403$q(electronic bk.)
035 $a(OCoLC)919150706
050 4 $aTA417.7.S5
082 04 $a620.11245$223
086 0 $aY 3.N 21/5:5/636
049 $aZCUA
100 1 $aKuhn, Paul.
245 10 $aApproximate stress analysis of multistringer beams with shear deformation of the flanges /$cby Paul Kuhn.
264 1 $aWashington, D.C. :$bU.S. Government Printing Office,$c1938.
300 $a1 online resource (ii, 21 pages) :$billustrations
336 $atext$btxt$2rdacontent
337 $acomputer$bc$2rdamedia
338 $aonline resource$bcr$2rdacarrier
490 1 $aReport / National Advisory Committee for Aeronautics ;$vnumber 636
504 $aIncludes bibliographical references (page 21).
588 0 $aPrint version record.
520 $aThe problem of the skin-stringer combinations used as axially loaded panels or as covers for box beams is considered from the point of view of the practical stress analyst. By a simple substitution the problem is reduced to the problem of the single-stringer structure, which has been treated in NACA Report no. 608. The method of making this substitution is essentially empirical; in order to justify it, comparisons are shown between calculations and strain-gage tests of three beams tested by the author and of one compression panel and three beams tested and reported elsewhere. --$cProvided by publisher.
650 0 $aShear (Mechanics)
650 0 $aDeformations (Mechanics)
650 0 $aStrains and stresses.
650 6 $aCisaillement (Mécanique)
650 6 $aDéformations (Mécanique)
650 6 $aContraintes (Mécanique)
650 7 $ashear stress.$2aat
650 7 $adeformation.$2aat
650 7 $aDeformations (Mechanics)$2fast$0(OCoLC)fst00889780
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.
710 1 $aUnited States.$bNational Advisory Committee for Aeronautics.
710 2 $aLangley Aeronautical Laboratory.
776 08 $iPrint version:$aKuhn, Paul.$tApproximate stress analysis of multistringer beams with shear deformation of the flanges$w(OCoLC)918949241
830 0 $aReport (United States. National Advisory Committee for Aeronautics) ;$vno. 636.
856 40 $uhttp://www.columbia.edu/cgi-bin/cul/resolve?clio11608457$zACADEMIC - Aerospace & Radar Technology
852 8 $blweb$hEBOOKS