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Volume 24 Issue 3
Mar.  1998
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Journal of Beijing University of Aeronautics and Astronautics  > 1998  >  24(3): 304-307.
XU Limin, ZHANG Tao, TAO Jiaweiet al. Energy-optimal and fuel-optimal problems for Lambert rendezvous[J]. Journal of Beijing University of Aeronautics and Astronautics, 2018, 44(9): 1888-1893. doi: 10.13700/j.bh.1001-5965.2017.0731(in Chinese)
Citation: Yan Chao, Xie Lei, Li Yunxiaoet al. Optimization Aerodynamic Design for Transonic Airfoil[J]. Journal of Beijing University of Aeronautics and Astronautics, 1998, 24(3): 304-307. (in Chinese)
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Optimization Aerodynamic Design for Transonic Airfoil

  • Beijing University of Aeronautics and Astronautics,Dept. of Flight Vehicle Design and Applied Mechanics

  • Received Date: 28 Jan 1997
  • Publish Date: 31 Mar 1998
    Abstract
  • Computational Fluid Dynamics(CFD) and optimization technique are combined in this paper for the purpose of optimal aerodynamic design of transonic airfoil. In this method, 2-D Euler equations are numerically solved to simulate the flow around airfoil using finite volume method, then geometric conditions, optimization equations are implemented to modify the airfoil through shape functions. The two steps are iterated until optimal aerodynamic performance of airfoil is achieved under certain conditions. Two cases, both based on the original airfoil of NACA0012, are presented to show the efficiency of this method.

     

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    • References(1)
  • 1 .Lee D. Application of computational fluid dynamics in transonic aerodynamic design.AIAA-93-3481-CP, 1993 2. Obayashi S, Takanashi S. Genetic optimization of target pressure distributions for inverse design methods.AIAA-95-1649-CP,1995 3. Reuther J, Jameson A. Control theory based airfoil design for potential flow and a finite volume discretization.AIAA-94-0499,1994 4. Lock R C. Aerodynamic design methods for transonic wings. Aeronautical J, 1990,94(1):1~16 5. Jameson, Schmidt W, Turkel F. Numerical solutions of the Euler equations by finite volume methods using Runge-Kutta time stepping schemes. AIAA-paper 81-1259,1981
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