Отрывок: 04,,,) COPPER_N = NODE (0.08,0,0) 17 STEEL_E = ENEARN (STEEL_N) COPPER_E = ENEARN (COPPER_N) ETABLE,STRS_ST,LS,1 ETABLE,STRS_CO,LS,1 *GET,STRSS_ST,ELEM,STEEL_E,ETAB,STRS_ST *GET,STRSS_CO,ELEM,COPPER_E,ETAB,STRS_CO Do the following calculation on your own: Fig. 3.4. Cantilevered beam The cantilevered, unevenly heated beam with square section is loaded with axial force F. Determine the maximum tensile stresses in the fixed-end, as well as th...
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dc.contributor.authorShklovets A. O.ru
dc.contributor.authorMinistry of Education and Science of the Russian Federationru
dc.contributor.authorSamara National Research University named after S. P. Korolev (Samara University)ru
dc.coverage.spatialучебные изданияru
dc.coverage.spatialметод конечных элементовru
dc.creatorShklovets A. O.ru
dc.date.issued2017ru
dc.identifierRU\НТБ СГАУ\415768ru
dc.identifier.citationShklovets, A. O. Work in CAE-package «Ansys Mechanical»: structural analysis by the finite element method [Электронный ресурс] : [electron textbook] / A. O. Shklovets ; Ministry of Education and Science of the Russian Federation, Samara National Research University named after S. P. Korolev(Samara University). - Samara, 2017. - on-lineru
dc.description.abstractThe tutorial describes the work in the software package for the finite element analysis Ansys. Examples of structural analysis for various structures are given. Calculations using beam, shell and volume finite elements are considered. The basic methods for creating the geometry of the model, generating a finite element mesh are described. Various types of loads applied in Ansys are described. This textbook is proposed for master students and bachelors of speciality 24.04.05, 24.03.05 «Aircraft Engines». Get ready at the Department of Construction and Design of Aircraft Engines.ru
dc.description.abstractТруды сотрудников Самар. ун-та (электрон. версия).ru
dc.description.abstractИспользуемые программы: Adobe Acrobat.ru
dc.description.abstractГриф.ru
dc.format.extentЭлектрон. дан. (1 файл : 2,84 Мб)ru
dc.language.isorusru
dc.titleWork in CAE-package «Ansys Mechanical»: structural analysis by the finite element methodru
dc.typeTextru
dc.subject.rugasnti27.23.19ru
dc.subject.udc621.432(075)ru
dc.textpart04,,,) COPPER_N = NODE (0.08,0,0) 17 STEEL_E = ENEARN (STEEL_N) COPPER_E = ENEARN (COPPER_N) ETABLE,STRS_ST,LS,1 ETABLE,STRS_CO,LS,1 *GET,STRSS_ST,ELEM,STEEL_E,ETAB,STRS_ST *GET,STRSS_CO,ELEM,COPPER_E,ETAB,STRS_CO Do the following calculation on your own: Fig. 3.4. Cantilevered beam The cantilevered, unevenly heated beam with square section is loaded with axial force F. Determine the maximum tensile stresses in the fixed-end, as well as th...-
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