Application of aeroelastic constraints in structural optimization-Reference-Cited by-同舟云学术

Application of aeroelastic constraints in structural optimization

Published:1969 Issue: Volume: Page:100-113
ISSN:
Container-title:Applied Mechanics
language:
Short-container-title:

Author:

Ashley H.,McIntosh S. C.

Publisher

Springer Berlin Heidelberg

Link

http://link.springer.com/content/pdf/10.1007/978-3-642-85640-2_7

Reference26 articles.

1. Schmit, L. A., W. M. Morrow and T. P. Richer: A Structural Synthesis Capability for Integrally Stiffened Cylindrical Shells, Paper No. 68–327, ’presented at AIAA/ASME 9th Structures, Structural Dynamics and Materials Conference, Palm Springs, Calif., April 1968.

2. Turner, M. J.: Design of Minimum Mass Structures with Specified Natural frequencies, AIAA J. 5, 406–412 (1967).

3. Ashley, H., and S. C. McIntosh: Expanding the Consciousness of the Aeroelastician, Proc. of ASME Symposium, Fluid-Solid Interaction, Pittsburgh, Nov. 1967, pp. 120–143.

4. McIntosh, S. C., and F. E. Eastep: Design of Minimum-Mass Structures with Specified Stiffness Properties, AIAA J. 6, 962–964 (1968).

5. Turner, M. J.: Optimization of Structures to Satisfy Flutter Requirements, unnumbered report of Commercial Airplane Division, The Boeing Co., 1968 (to appear in AIAA J.).

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