Reduced-Order Design-Oriented Stress Analysis Using Combined Direct and Adjoint Solutions-Reference-Cited by-同舟云学术

Reduced-Order Design-Oriented Stress Analysis Using Combined Direct and Adjoint Solutions

Published:2000-05 Issue:5 Volume:38 Page:898-909
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Livne Eli¹,Blando Guillermo D.¹

Affiliation:

1. University of Washington, Seattle, Washington 98195-2400

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/2.1045

Reference37 articles.

1. Bisplinghoff, R. L., Ashley, H., and Halfman, R. L., Aeroelasticity, Addison Wesley Longman,Reading, MA, 1955, pp.641-650; alsoDover, New York, 1996.

2. Hurty, W. C., and Rubinstein, M. F., Dynamics of Structures, Prentice-Hall, Englewood Cliffs, NJ, 1964, pp.299-307.

3. Reduction of stiffness and mass matrices

4. Automatic choice of global shape functions in structural analysis

5. Coupling of substructures for dynamic analyses.

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