Dynamic stress analysis of rotating turbo-machinery bladed-disk systems
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Publication:3474965
DOI10.1016/0045-7949(89)90057-6zbMath0697.73057OpenAlexW1969806516MaRDI QIDQ3474965
Publication date: 1989
Published in: Computers & Structures (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1016/0045-7949(89)90057-6
triangular shell elementLove-Kirchhoff hypothesissix degrees of freedom per nodeblade and disk attachmenthigh pressure stageinitial stress and membrane behaviourone substructureout of core submatrices elimination methodrotational periodicityset of constraint equations
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