MARC Record from marc_columbia

LEADER: 03229cam a2200661 i 4500
001 11608395
005 20220514224414.0
006 m o d f
007 cr |||||||||||
008 150719e194706 dcuad obt f000 0 eng d
035 $a(OCoLC)ocn914158513
035 $a(NNC)11608395
040 $aSINTU$beng$erda$epn$cSINTU$dSINTU$dOCLCO$dKNOVL$dZCU$dOCLCQ$dUAB$dDKU$dOCLCF$dOCLCQ$dCEF$dRRP$dWYU$dYOU$dS2H$dOCLCO$dCOP$dOCLCO$dCOP$dOCLCO
019 $a951667875
020 $a9781680156041$q(electronic bk.)
020 $a1680156047$q(electronic bk.)
035 $a(OCoLC)914158513$z(OCoLC)951667875
050 4 $aTA660.S5
082 04 $a624.17762$223
086 0 $aY 3.N 21/5:6/1344
088 $aNACA-TN-1344
049 $aZCUA
100 1 $aBatdorf, S. B.,$eauthor.
245 10 $aCritical stress of thin-walled cylinders in torsion /$cby S.B. Batdort, Manuel Stein and Murry Schildcrout.
264 1 $aWashington, D.C. :$bNational Advisory Committee for Aeronautics,$c1947.
300 $a1 online resource (21, [5] pages) :$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. 1344
500 $a"Langley Memorial Aeronautical Laboratory."
500 $aDate of issue: June 1947.
500 $aReport no. NACA TN No. 1344.
504 $aIncludes bibliographical references (page 19)
520 3 $aA theoretical solution is given of the critical stress of thin-walled cylinders loaded in torsion. The results are presented in terms of a few simple formulas and curves which are applicable to a wide range of cylinder dimensions from very short cylinders of large radius to long cylinders of small radius. Theoretical results are found to be in somewhat better agreement with experimental results than previous theoretical work for the same range of cylinder dimensions.
588 0 $aPrint version record.
650 0 $aShells (Engineering)$xThin-walled structures.
650 0 $aCylinders.
650 0 $aStrains and stresses.
650 0 $aTorsion.
650 6 $aCylindres.
650 6 $aContraintes (Mécanique)
650 6 $aTorsion (Mécanique)
650 7 $acylinders (solids)$2aat
650 7 $atorsional stress.$2aat
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 $aStein, Manuel,$eauthor.
700 1 $aSchildcrout, Murry,$eauthor.
710 1 $aUnited States.$bNational Advisory Committee for Aeronautics,$eissuing body.
710 2 $aLangley Aeronautical Laboratory.
776 08 $iPrint version:$aBatdorf, S.B.$tCritical stress of thin-walled cylinders in torsion.$dWashington, D.C. : National Advisory Committee for Aeronautics, 1947$w(OCoLC)652531296
830 0 $aTechnical note (United States. National Advisory Committee for Aeronautics) ;$vno. 1344.
856 40 $uhttp://www.columbia.edu/cgi-bin/cul/resolve?clio11608395$zACADEMIC - Aerospace & Radar Technology
852 8 $blweb$hEBOOKS