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跨音速翼型
1、In this paper, the optimization design of the transonic airfoil is performed by the Response Surface Methodology(RSM).───基于响应面方法进行了跨声速翼型的气动优化设计。
2、Optimization Aerodynamic Design for Transonic Airfoil───跨音速翼型的气动最优化设计方法
3、variational of finite element method(FEM) using the pseudo-potential function is presented to design the airfoil shape of transonic rotational flows.───运用赝势函数变域变分有限元方法进行了跨音速翼型设计。
4、Sidewall Effects and Suction Technique in Two-Dimensional Transonic Airfoil Wind Tunnel Test───二元翼型风洞的侧壁干扰与抽气研究
5、displayed that the testing technique of flexible adaptive walled wind tunnel could apply to future transonic airfoil testing.───实验结果展示了自适应壁风洞实验技术用于翼型跨音速实验的前景。
6、Hierarchial Evolutionary Algorithms and Its Application in Transonic Airfoil Optimization in Aerodynamics───分级型进化算法及其在翼型跨声速气动优化中的应用
7、transonic flow field around NACA 0012 airfoil is calculated by finite element method from pressure minimum integration, full potential equation being used.───有限元法计算了NACA 0012翼型的跨音速流场。出发方程为全速位方程。
8、Numerical results show that the method provides an effective tool for refining and designing a transonic airfoil.───算例结果表明，本方法提供了一种跨音速翼型改型设计及新翼型设计的有效工具。
9、It is further displayed that the testing technique of flexible adaptive walled wind tunnel could apply to future transonic airfoil testing.───实验结果展示了自适应壁风洞实验技术用于翼型跨音速实验的前景。
1、An effective aerodynamic optimization design method of transonic airfoil is given.