It looks like you're offline.
Open Library logo
additional options menu

MARC Record from marc_columbia

Record ID marc_columbia/Columbia-extract-20221130-024.mrc:62006498:3689
Source marc_columbia
Download Link /show-records/marc_columbia/Columbia-extract-20221130-024.mrc:62006498:3689?format=raw

LEADER: 03689cam a2200769 i 4500
001 11608396
005 20220423224546.0
006 m o d f
007 cr |||||||||||
008 150722s1947 dcuad obt f000 0 eng d
035 $a(OCoLC)ocn914248233
035 $a(NNC)11608396
040 $aSINTU$beng$erda$epn$cSINTU$dSINTU$dOCLCO$dSINTU$dKNOVL$dZCU$dOCLCQ$dUAB$dDKU$dOCLCF$dOCLCQ$dCEF$dRRP$dUMR$dMERER$dWYU$dOCLCQ$dYOU$dOCL$dS2H$dOCLCO$dCOP$dOCLCO$dCOP$dOCLCO
019 $a951667856
020 $a9781680156058$q(electronic bk.)
020 $a1680156055$q(electronic bk.)
035 $a(OCoLC)914248233$z(OCoLC)951667856
050 4 $aTA660.S5
082 04 $a624.17762$223
086 0 $aY 3.N 21/5:6/1345
088 $aNACA-TN-1345
049 $aZCUA
100 1 $aBatdorf, S. B.,$eauthor.
245 10 $aCritical combinations of torsion and direct axial stress for thin-walled cylinders /$cby S.B. Batdort, Manuel Stein and Murry Schildcrout.
264 1 $aWashington, D.C. :$bNational Advisory Committee for Aeronautics,$c1947.
300 $a1 online resource (28, [8] pages) :$billustrations, tables.
336 $atext$btxt$2rdacontent
337 $acomputer$bc$2rdamedia
338 $aonline resource$bcr$2rdacarrier
490 1 $aNational Advisory Committee for Aeronautics technical note ;$vno. 1345
500 $a"Langley Memorial Aeronautical Laboratory."
500 $aDate of issue: June 1947.
500 $aReport no. NACA TN No. 1345.
504 $aIncludes bibliographical references (page 25)
520 3 $aA theoretical solution is presented for the determination of the combinations of direct axial stress and torsion which cause thin-walled cylinders with either simply supported or clamped edges to buckle. This theoretical solution is used in conjunction with available test data to develop empirical curves and formulas for use in design. Comparisons are made with theoretical and empirical solutions obtained in other investigations.
588 0 $aPrint version record.
650 0 $aShells (Engineering)
650 0 $aThin-walled structures.
650 0 $aCylinders.
650 0 $aStrains and stresses.
650 0 $aTorsion.
650 0 $aBuckling (Mechanics)
650 6 $aCoques (Ingénierie)
650 6 $aStructures à parois minces.
650 6 $aCylindres.
650 6 $aContraintes (Mécanique)
650 6 $aTorsion (Mécanique)
650 6 $aFlambage (Résistance des matériaux)
650 7 $ashell structures.$2aat
650 7 $acylinders (solids)$2aat
650 7 $atorsional stress.$2aat
650 7 $aThin-walled structures.$2fast$0(OCoLC)fst01150059
650 7 $aShells (Engineering)$2fast$0(OCoLC)fst01115734
650 7 $aBuckling (Mechanics)$2fast$0(OCoLC)fst00840001
650 7 $aCylinders.$2fast$0(OCoLC)fst00886041
650 7 $aStrains and stresses.$2fast$0(OCoLC)fst01134288
650 7 $aTorsion.$2fast$0(OCoLC)fst01152860
655 0 $aElectronic books.
655 4 $aElectronic books.
700 1 $aStein, Manuel.
700 1 $aSchildcrout, Murry.
710 1 $aUnited States.$bNational Advisory Committee for Aeronautics,$eissuing body.
710 2 $aLangley Aeronautical Laboratory.
776 08 $iPrint version:$aBatdorf, S.B.$tCritical combinations of torsion and direct axial stress for thin-walled cylinders.$dWashington, D.C. : National Advisory Committee for Aeronautics, 1947$w(OCoLC)652531421
830 0 $aTechnical note (United States. National Advisory Committee for Aeronautics) ;$vno. 1345.
856 40 $uhttp://www.columbia.edu/cgi-bin/cul/resolve?clio11608396$zACADEMIC - Aerospace & Radar Technology
852 8 $blweb$hEBOOKS