| Record ID | marc_columbia/Columbia-extract-20221130-024.mrc:62246369:4071 |
| Source | marc_columbia |
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LEADER: 04071cam a2200793 i 4500
001 11608465
005 20221203224052.0
006 m o d
007 cr cnu---unuuu
008 150825s1935 dcua obt f000 0 eng d
035 $a(OCoLC)ocn919168137
035 $a(NNC)11608465
040 $aKNOVL$beng$erda$epn$cKNOVL$dOCLCE$dZCU$dOCLCQ$dUAB$dDKU$dOCLCQ$dCEF$dRRP$dYOU$dS2H$dOCLCO$dOCLCQ$dUPM
019 $a297432259$a608168843$a977309390$a987643080$a1047743383$a1229061459
020 $a9781680156577$q(electronic bk.)
020 $a1680156578$q(electronic bk.)
035 $a(OCoLC)919168137$z(OCoLC)297432259$z(OCoLC)608168843$z(OCoLC)977309390$z(OCoLC)987643080$z(OCoLC)1047743383$z(OCoLC)1229061459
042 $adlr
050 4 $aTA660.S5
082 04 $a624.17762$223
086 0 $aY 3.N 21/5:8/774
088 $aNACA TM 774
049 $aZCUA
100 1 $aWagner, H.,$eauthor.
245 10 $aTension fields in originally curved, thin sheets during shearing stresses /$cH. Wagner and W. Ballerstedt.
264 1 $aWashington, D.C. :$bNational Advisory Commitee for Aeronautics,$c[1935]
300 $a1 online resource (11 pages, 2 unnumbered pages) :$billustrations
336 $atext$btxt$2rdacontent
337 $acomputer$bc$2rdamedia
338 $aonline resource$bcr$2rdacarrier
490 1 $aTechnical memorandums ;$vnumber 774
500 $a"August 1935."
500 $aNACA TM No. 774.
500 $aTranslated from Luftfahrtforschung. Vol. 12, No. 2, pp. 70-74, May 16, 1935, by the National Advisory Commitee for Aeronautics.
504 $aIncludes bibliographical references.
520 3 $aThe analysis of the stresses in the sheet and stiffeners is predicated upon the direction of the wrinkles, particularly the tensile stresses (principal stresses). This analysis and the calculation of stresses after buckling form the subject of the present article. It includes: 1) metal cylinders with closely spaced longitudinal stiffeners; 2) metal cylinders with closely spaced transverse rings.
588 0 $aPrint version record.
506 $3Use copy$fRestrictions unspecified$2star$5MiAaHDL
533 $aElectronic reproduction.$b[Place of publication not identified] :$cHathiTrust Digital Library,$d2010.$5MiAaHDL
538 $aMaster and use copy. Digital master created according to Benchmark for Faithful Digital Reproductions of Monographs and Serials, Version 1. Digital Library Federation, December 2002.$uhttp://purl.oclc.org/DLF/benchrepro0212$5MiAaHDL
583 1 $adigitized$c2010$hHathiTrust Digital Library$lcommitted to preserve$2pda$5MiAaHDL
506 $aAccess restricted to Ryerson students, faculty and staff.$5CaOTR
650 0 $aShells (Engineering)
650 0 $aThin-walled structures.
650 0 $aCurvature.
650 0 $aShear (Mechanics)
650 0 $aStrains and stresses.
650 6 $aCoques (Ingénierie)
650 6 $aStructures à parois minces.
650 6 $aCourbure.
650 6 $aCisaillement (Mécanique)
650 6 $aContraintes (Mécanique)
650 7 $ashell structures.$2aat
650 7 $ashear stress.$2aat
650 7 $astrain.$2aat
650 7 $astress.$2aat
650 7 $aCurvature.$2fast$0(OCoLC)fst00885436
650 7 $aShear (Mechanics)$2fast$0(OCoLC)fst01115422
650 7 $aShells (Engineering)$2fast$0(OCoLC)fst01115734
650 7 $aStrains and stresses.$2fast$0(OCoLC)fst01134288
650 7 $aThin-walled structures.$2fast$0(OCoLC)fst01150059
655 0 $aElectronic books.
655 4 $aElectronic books.
700 1 $aBallerstedt, W.,$eauthor.
710 1 $aUnited States.$bNational Advisory Commitee for Aeronautics.
776 08 $iPrint version:$aWagner, H.$tTension fields in originally curved, thin sheets during shearing stresses$w(OCoLC)696180837
830 0 $aTechnical memorandum (United States. National Advisory Committee for Aeronautics) ;$vno. 774.
856 40 $uhttp://www.columbia.edu/cgi-bin/cul/resolve?clio11608465$zACADEMIC - Aerospace & Radar Technology
852 8 $blweb$hEBOOKS