Optimum design of aircraft thin-walled structures

• Autorzy: Safronov V. , Turkin I.
• Konferencja: Proceedings of the Fourth Seminar on Recent Research and Design Progress in Aeronautical Engineering and its Influence on Education/seminar(IV; 30.11-02.12.2000; Warszawa, Polska)
• Języki publikacji: EN

Abstrakty

EN

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.

Słowa kluczowe

EN

aircrafts; optimization; gradient methods

PL

samoloty; optymalizacja; metody gradientowe

• Wydawca: Institute of Aeronautics and Applied Mechanics, Warsaw University of Technology
• Czasopismo: Research Bulletin / Warsaw University of Technology, Institute of Aeronautics and Applied Mechanics
• Rocznik: 2001
• Tom: nr 12
• Strony: 69--72
• Opis fizyczny: Bibliogr. 6 poz., rys., tab., wykr.

Twórcy

autor

Safronov V.

autor

Turkin I.

• Moscow State Aviation Institute - Technical University, Moscow, Russia,