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。
transonic airfoil（英语使用场景）
1、An effective aerodynamic optimization design method of transonic airfoil is given.
transonic airfoil（意思翻译）
跨音速翼型
transonic airfoil（双语使用场景）
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。
transonic airfoil（英语使用场景）
1、An effective aerodynamic optimization design method of transonic airfoil is given.