Optimal design of composite wing subjected to gust loads
Author:
Publisher
Elsevier BV
Subject
Computer Science Applications,Mechanical Engineering,General Materials Science,Modeling and Simulation,Civil and Structural Engineering
Reference17 articles.
1. Preliminary design of composite wings for buckling, strength, and displacement constraints;Starnes;J Aircraft,1979
2. An efficient structural resizing procedure for meeting static aeroelastic design objectives;Lerner;J Aircraft,1979
3. Optimum design of composite wing structures by a refined optimality criterion;Liu;Compos Struct,1991
4. Two-level composite wing structural optimization using response surface;Liu;Struct Multidisc Optimiz,2000
5. Aeroelastic tailoring of composite structures;Eastep;J Aircraft,1999
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