Optimal Design of Grid-Stiffened Composite Panels
Author:
Affiliation:
1. Old Dominion University, Norfolk, Virginia 23529-0247
2. NASA Langley Research Center, Hampton, 23681-0001
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.2321
Reference29 articles.
1. Optimization of laminate stacking sequence for buckling load maximization by genetic algorithm
2. DESIGN OF A BLADE STIFFENED COMPOSITE PANEL BY GENETIC ALGORITHM
3. 4Whitney, S. A. “Formulation of Genetic Algorithm for Solution of Engineering Designs,” M.S. Thesis, Aerospace Engineering Dept.Old Dominion Univ., Norfolk, VA,May 1995.
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