LEADER 01187nam a2200289 i 4500 001 991001895119707536 005 20020508183411.0 008 971203s1997 de ||| | ger 020 $a3519074303 035 $ab10928777-39ule_inst 035 $aPARLA150771$9ExL 040 $aDip. di Filol. Class. e di Scienze Filosofiche$bita 082 0 $a888 100 1 $aEbert, Joachim$0189772 245 10$aAgonismata :$bKleine philologische Schriften zur Literatur, Geschichte und Kultur der Antike /$cJoachim Ebert ; Herausgegeben von Michael Hillgruber, Rainer Jakobi und Wolfgang Luppe unter Mitarbeit von Marcus Beck und Rainer Lenk 260 $aStuttgart ; Leipzig :$bTeubner,$c1997 300 $aviii, 431 p. ;$c24 cm. 650 4$aCultura classica$xStudi 650 4$aEbert, Joachim - Scritti minori 650 4$aLetteratura classica$xStudi 650 4$aStoria antica$xStudi 907 $a.b10928777$b21-09-06$c28-06-02 912 $a991001895119707536 945 $aLE007 M 1648$g1$i2007000048610$lle007$o-$pE0.00$q-$rn$so $t0$u0$v0$w0$x0$y.i11033514$z28-06-02 996 $aAgonismata$9920079 997 $aUNISALENTO 998 $ale007$b01-01-97$cm$da $e-$fger$gde $h0$i1 LEADER 02700oam 2200733I 450 001 9910709797103321 005 20180614135925.0 035 $a(CKB)5470000002472271 035 $a(OCoLC)785231981$z(OCoLC)761278728 035 $a(EXLCZ)995470000002472271 100 $a20120408j198503 ua 0 101 0 $aeng 135 $aurbn||||||abp 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aLocal strain redistribution corrections for a simplified inelastic analysis procedure based on an elastic finite-element analysis /$fAlbert Kaufman and Shoi Y. Hwang 210 1$aWashington, D.C. :$cNational Aeronautics and Space Administration, Scientific and Technical Information Branch,$dMarch 1985. 215 $a1 online resource (11 pages) $cillustrations 225 1 $aNASA/TP ;$v2421 300 $a"March 1985." 320 $aIncludes bibliographical references (page 11). 606 $aAircraft gas-turbines$xMaterials 606 $aElastic analysis (Engineering) 606 $aFinite element method 606 $aStrains and stresses 606 $aAircraft gas-turbines$xMaterials$2fast 606 $aElastic analysis (Engineering)$2fast 606 $aFinite element method$2fast 606 $aStrains and stresses$2fast 606 $aCyclic loads$2nasat 606 $aFinite element method$2nasat 606 $aInelastic stress$2nasat 606 $aNonlinear equations$2nasat 606 $aStress distribution$2nasat 606 $aStress-strain relationships$2nasat 615 0$aAircraft gas-turbines$xMaterials. 615 0$aElastic analysis (Engineering) 615 0$aFinite element method. 615 0$aStrains and stresses. 615 7$aAircraft gas-turbines$xMaterials. 615 7$aElastic analysis (Engineering) 615 7$aFinite element method. 615 7$aStrains and stresses. 615 7$aCyclic loads. 615 7$aFinite element method. 615 7$aInelastic stress. 615 7$aNonlinear equations. 615 7$aStress distribution. 615 7$aStress-strain relationships. 700 $aKaufman$b Albert$f1928-$01413652 702 $aHwang$b Shoi Y. 712 02$aUnited States.$bNational Aeronautics and Space Administration.$bScientific and Technical Information Branch, 801 0$bOCLCE 801 1$bOCLCE 801 2$bOCLCQ 801 2$bOCLCO 801 2$bOCLCF 801 2$bOCLCQ 801 2$bGPO 906 $aBOOK 912 $a9910709797103321 996 $aLocal strain redistribution corrections for a simplified inelastic analysis procedure based on an elastic finite-element analysis$93526440 997 $aUNINA