Finally, the effect of incoming flow to isolator’s performance is studied.
最后研究了来流条件对隔离段性能的影响。
参考来源 - 非常规隔离段流场特征与气动性能的数值研究In order to investigate the characteristics of wall pressure fluctuations in a rectangled isolator, wind tunnel experiments were performed on the isolator using wall pressure fluctuation measurements and statistically analysis.
为了探讨非对称来流下矩形隔离段内动态压力特性,用直联实验方式以及动态压力测量技术进行了试验,并用统计分析方法分析了数据,得出了非对称来流下隔离段壁面压力脉动动态特性。
参考来源 - 非对称来流下隔离段流动特性研究·2,447,543篇论文数据，部分数据来源于NoteExpress
研究发现，在不同反压下隔离段中的平均马赫数和平均压力值，从隔离段进口到激波串波前基本保持不变。
It was observed that the average values of Mach Numbers and pressures were almost constant from the entrance of the isolator to the onset of shock train along the isolator.
在计算中用一维、定比热容方法分析了相关参数对燃烧室模态转变、性能的影响和隔离段与燃烧室的相互作用。
One dimensional constant specific heat model was taken to analyze the influence of the related parameters on the combustion mode transition and the combustor performance.
侧板后掠角大小和整流罩位置变化时，对进气道的质量捕获、总压恢复系数和隔离段出口流场的均匀性等都有一定的影响。
Changes of sidewall sweep Angle and cowl position can influence inlet performance such as mass capture, total pressure recovery coefficient and uniformity of isolator exit flow field.
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