In this paper, a new iterative testing strategy is described for two dimensional model testing in transonic flexible adaptive walled wind tunnel and wall adjustment computing method.
给出一种新的二维跨音速柔性自适应壁风洞实验迭代方案，计算方法和实验验证结果。
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It is further displayed that the testing technique of flexible adaptive walled wind tunnel could apply to future transonic airfoil testing.