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A modal aeroelastic finite element analysis method for advanced turbomachinery stages

โœ Scribed by G. Jacquet-Richardet; R. Henry


Publisher
John Wiley and Sons
Year
1994
Tongue
English
Weight
737 KB
Volume
37
Category
Article
ISSN
0029-5981

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A new "rst-order formulation for the two-dimensional elasticity equations is proposed by introducing additional variables which, called stresses here, are the derivatives of displacements. The resulted stress}displacement system can be further decomposed into two dependent subsystems, the stress sys