Optimization of Flat Z-stiffened Panel Subjected to Compression
Author:
Affiliation:
1. Aerospace Systems Company, Kawasaki Heavy Industries, Ltd.
Publisher
Japan Society for Aeronautical and Space Sciences
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://www.jstage.jst.go.jp/article/tjsass/62/1/62_T-18-6/_pdf
Reference12 articles.
1. 1) Niu, M. C.: Aircraft Structural Design, Conmilt Press Ltd., Hong Kong, 1989.
2. 2) Farrar, D. J.: The Design of Compression Structures for Minimum Weight, J. Royal Aeronautical Soc., 53 (1949), pp. 1041–1052.
3. 3) Initial Buckling Stress of Flat Panels with Z-section Stringers under Compression, ESDU, 02.01.25, 1947.
4. 4) Williams, J. G. and Stein, M.: Buckling Behavior and Structural Efficiency of Open-Section Stiffened Composite Compression Panels, AIAA J., 14, 11 (1976), pp. 1618–1626.
5. 5) Bushnell, D.: Optimization of Panels with Riveted Z-shaped Stiffeners Via PANDA2, AIAA-98-1990, 39th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit, 1998, pp. 2357–2388.
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