Shear and compression buckling analysis for anisotropic panels with elliptical cutouts-Reference-Cited by-同舟云学术

Shear and compression buckling analysis for anisotropic panels with elliptical cutouts

Published:1994-11 Issue:11 Volume:32 Page:2293-2299
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Britt V. O.¹

Affiliation:

1. NASA Langley Research Center, Hampton, Virginia 23681

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.12289

Reference11 articles.

1. Buckling of Laminated Plates with Holes

2. Optimum design of cutouts in laminated composite structures

3. 4Nemeth, M. P. "Buckling Behavior of Orthotropic Composite Plates with Centrally Located Cutouts," Ph.D. Dissertation, Virginia Polytechnic Inst.and State Univ., Blacksburg, VA,May 1983.

4. Owen, V. L. "Shear Buckling of Anisotropic Plates with Centrally Located Circular Cutouts," M.S. Thesis,North Carolina State Univ., Raleigh, NC, May 1990.

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