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。
This paper is a report of experimental pressure. Measurement research for NACA0012 airfoil in NH-1 transonic wind tunnel.
本文为NACA0012翼型在NH - 1风洞进行跨音速二维测压实验的研究报告。
The variational of finite element method(FEM) using the pseudo-potential function is presented to design the airfoil shape of transonic rotational flows.
本文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。
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