以下为句子列表：
英文: The profiles of density, velocity, temperature, pressure and Mach number can be obtained by the computation.
中文: 通过计算可以得出密度、速度、温度、压力和马赫数的分布。
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英文: The results prove that: (1) When the Mach number of the flow at the exit increases, the total pressure recovery decreases, and the circular steady total pressure distortion coefficient, turbulence intensity and synthesis distortion increase.
中文: 研究结果表明：(1)地面工作状态下，随着出口马赫数的增加，蛇形进气道出口截面的总压恢复系数不断下降，而稳态周向畸变指数、紊流度和综合畸变指数均上升，稳态径向畸变指数变化不大。
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英文: Variations in pressure with and without aeration in cavitation region are measured and the compressible characteristics of pressure waveforms and relation between Mach number and compression ratio are analyzed; the time-averaged pressure profiles of diffe
中文: 实测了空化区掺气前后压力的变化，分析了压力波形的可压缩流特征以及马赫数与压缩比的关系；实测了空蚀区不同掺气浓度的时均压力分布，分析了压力随掺气浓度的变化及背压对空蚀的影响；提出减免空蚀的最低掺气浓度与流速的关系，比较了掺气前后水流的空化数。
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英文: When the serpentine inlet is running at the exit Mach number Ma(subscript e)=0.45, the total pressure recovery coefficient equals 0.90, and synthesis distortion equals 13.85%.
中文: 本研究的蛇形进气道在出口马赫数为0.45时，总压恢复系数为0.90，综合畸变指数为13.85%，总压恢复较低，畸变较大，超出了一般航空发动机的承受范围。
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英文: The Mach number Ma =0. and the Reynold number Re = 0000 are used in the computation.
中文: 给出了Ma_∞=0. ,0.8;
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