Optimization design of wing-s thickness and twist angle using Euler equations

[1] Van der Velden A, Forbrich D. Use of aerodynamic shape optimization for a large transonic aircraft . AIAA 97-2274,1997 [2] Van der Velden A, Von Reith D. Multi-disciplinary SCT design at deutsche aerospace airbus Proceedings of the 7^th European Aerospace Conference, Toulouse:,1994 [3] Takahashi T T, Coopersmith R M. Wing section design for a long-range hydrofoil transport . AIAA 2002-0832,2002 [4] Sobieczky H. New design concept for high speed air transports CISM cours and Lectures NO.366. New York:Springer Wien,1997 [5]  朱自强,吴宗成.现代飞机设计空气动力学[M].北京:北京航空航天大学出版社,2005 Zhu Ziqiang, Wu Zongcheng. Aerodynamics for modern aircraft design[M]. Beijing:Beijing University of Aeronautics and Astronautics Press,2005(in Chinese) [6]  Jameson A, Schmidt W, Turkel E. Numerical solutions of the Euler equations by finite volume methods with Runge-Kutta time stepping schemes . AIAA 81-1259,1981 [7] Powell M J D. An efficient method for finding the minimum of a function of several variables without calculation derivatives[J]. Computer Journal, 1964, 7:155-162 [8] Burdges K P, Hinson B L. Transport wing and far field test data on a moderate aspect ratio wing for three dimensional computational method evaluation . AGARD-AR-138,1979