Volume 34 Issue 02
Feb.  2008
Turn off MathJax
Article Contents
Wen Jianhua, Zhu Ziqiang, Wu Zongcheng, et al. Wing-s optimization design using serial and parallel computations based on N-S equations[J]. Journal of Beijing University of Aeronautics and Astronautics, 2008, 34(02): 127-130. (in Chinese)
Citation: Wen Jianhua, Zhu Ziqiang, Wu Zongcheng, et al. Wing-s optimization design using serial and parallel computations based on N-S equations[J]. Journal of Beijing University of Aeronautics and Astronautics, 2008, 34(02): 127-130. (in Chinese)

Wing-s optimization design using serial and parallel computations based on N-S equations

  • Received Date: 29 Jan 2007
  • Publish Date: 29 Feb 2008
  • The serial and parallel flow field solution program was validated at two Mach numbers between 0.7 and 0.9 using both a high and a moderate aspect ratio wings. The result based on the Navier-Stokes(N-S) equations proved it right and the parallel efficiency as well as speed-up ratio was discussed. With the goal of maximizing lift-to-drag ratio, the optimization of three-dimensional wing-s section thickness and twist angle was discussed. N-S equations as flow field sovler and Powell method were used as design tools, and the wing-s aspect shape was fixed. The subcritical parallel computation case and supercritical serial computation case demonstrated that nonlinear distribution of thickness and negative twist angle could ameliorate the condition of flow field around the wing, which lead to a higher lift-to-drag ratio. The optimization method is effective.

     

  • loading
  • [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 7th 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 Sobieczky H. 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] Lion M S. Progress towards an improved CFD method: AUSM+ . AIAA, 95-1701,1995 [7] 李岩,朱自强,王晓璐,等.基于Euler方程的三维机翼厚度与扭角优化设计[J].北京航空航天大学学报,2007,33(3):269-272 Li Yan, Zhu Ziqiang, Wang Xiaolu, et al. Optimization design of wing’s thickness and twist angle using Euler equations[J]. Journal of Beijing University of Aeronautics and Astronautics, 2007,33(3):269-272(in Chinese) [8] Burdges K P, Hinson B L. Transport wing and far field test data on a high aspect ratio wing for three dimensional computational method evaluation . AGARD-AR-138,1979 [9] 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
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索

    Article Metrics

    Article views(3970) PDF downloads(1415) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return