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Optimum design of aircraft thin-walled structures

Safronov V., Turkin I.

Research Bulletin / Warsaw University of Technology, Institute of Aeronautics and Applied Mechanics

2001

nr 12

69-72

The optimum design methodology of aircraft thin-walled shell structures at complex loading is presented in this article. The optimization of a thin'walled structure is performed to criterion of minor mass with using of the developed modified method for gradient projection on strength, stability and reliability of a thin-walled structure in statics and dynamics, and also in view of technological and operational limitations. The results of a sample test are shown in this article as well.