In this paper, a new iterative testing strategy is described for two dimensional model testing in transonic flexible adaptive walled windtunnel 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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FL-7 is a continuous transonic windtunnel, which is powered by three engines. Mach number is adjusted by the rotating speed of engines, the flexiblewall nozzle and the by-pass valve.
FL-7 is a continuous transonic windtunnel, which is powered by three engines. Mach number is adjusted by the rotating speed of engines, the flexiblewall nozzle and the by-pass valve.