It is further displayed that the testing technique of flexible adaptive walled wind tunnel could apply to future transonicairfoil 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。
2
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。
3
The variational of finite element method(FEM) using the pseudo-potential function is presented to design the airfoil shape of transonic rotational flows.