Stacking sequence optimization of simply supported laminates with stability and strain constraints

Author:

NAGENDRA S.1,HAFTKA R.1,GURDAL Z.1

Affiliation:

1. Virginia Polytechnic Institute and State University, Blacksburg

Publisher

American Institute of Aeronautics and Astronautics

Reference31 articles.

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2. Difficulties in Optimization of Imperfect Stiffened Cylindrical Shells;47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference<BR> 14th AIAA/ASME/AHS Adaptive Structures Conference<BR> 7th;2006-05

3. Optimization of panels with riveted Z-shaped stiffeners via PANDA2;39th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit;1998-04-20

4. Approximate method for the optimum design of ring and stringer stiffened cylindrical panels and shells with local, inter-ring, and general buckling modal imperfections;35th Structures, Structural Dynamics, and Materials Conference;1994-04-18

5. OPTIMUM DESIGN OF COMPOSITE STIFFENED PANELS UNDER COMBINED LOADING;34th Structures, Structural Dynamics and Materials Conference;1993-04-19

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