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Experimental Study of Moving Throat Plug in a Shock Tunnel

机译:冲击波隧道动喉塞的实验研究。

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Shock tunnel experiments are conducted to investigate the shock tunnel nozzle flow affected by a moving throat plug. In this experimental study the moving throat plug terminates the shock tunnel nozzle flow after the steady flow is finished. For the flow values in the steady state, there exists a negligible difference between the moving throat plug and the stationary throat plug.
机译:进行了冲击隧道实验,以研究受活动喉塞影响的冲击隧道喷嘴流量。在此实验研究中,在稳定流完成后,活动喉咙塞终止了冲击通道喷嘴的流。对于稳态下的流量值,活动式喉塞和固定式喉塞之间的差异可忽略不计。

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