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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 1998, Vol. 19 ›› Issue (1): 83-86.
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Zubair Islam, Zhu Yikun, Zhu Ziqiang, Xue Xiaochun
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Abstract:
An effective aerodynamic optimization design method of transonic airfoil is given. The numerical solution of Euler equations is provided as flowsolver. Both direct and indirect optimization methods are used for the optimization with constraints. Numerical results show that the method provides an effective tool for refining and designing a fransonic airfoil.
Key words: aer odynamic optimizat ion design, transonic airfoil, Euler equat ion
CLC Number:
V211.3
V244
Zubair Islam;Zhu Yikun;Zhu Ziqiang;Xue Xiaochun. AERODYNAMIC OPTIMIZATION DESIGN METHOD OF TRANSONIC AIRFOIL[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1998, 19(1): 83-86.
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