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Application results for new adaptive control system for working gas pressure in supersonic periodical wind tunnel pretest chamber

机译:超音速周期风洞采用新型自适应控制系统的应用结果

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The airflow control system for supersonic periodical wind tunnel (WT) supposed. New internal model regulator (IMC [5]) is used to improve pretest chamber pressure P_0 prohibitive over-regulation detected for "large" Mach numbers (M > 2.3). Verification test in situ have been performed for M = 3.0, 3.5. Results for the new regulator implementation shown.
机译:超音速定期风洞(WT)的气流控制系统假定。新型内部模型调节器(IMC [5])用于改善预测的腔室压力P_0,对“大”马赫数(M> 2.3)检测到检测到的过度调节。已经为M = 3.0,3.5执行了原位的验证测试。结果显示了新的调节器实现。

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