| 变唇口型总压畸变流场的模拟技术 |
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| 引用本文： | 陈晓,毛建.变唇口型总压畸变流场的模拟技术[J].航空动力学报,1990,5(1):57-64,92-93. |
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| 作者姓名： | 陈晓 毛建 |
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| 作者单位： | Nanjing Aeronautical Institute |
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| 摘 要： | 本文对变唇口型总压畸变流场模拟技术进行了试验研究。一方面总结分析了各种唇口几何参数对总压分布谱图和总压脉动紊流度的影响, 从而将这些一般的规律应用于特定总压分布谱图, 总压脉动紊流度及其畸变指数的模拟。另一方面, 对给定的二个不同类型的总压畸变流场进行模拟, 所模拟的稳态周向总压畸变指数, 平均总压脉动紊流度和最大瞬时畸变指数均能达到规定偏差的要求。
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| 收稿时间： | 8/1/1989 12:00:00 AM |
TECHNIQUE OF VARYING-LIP SIMULATING TOTAL PRESSURE DISTORTED FLOW FIELD |
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| Chen Xiao and Mao Jian.TECHNIQUE OF VARYING-LIP SIMULATING TOTAL PRESSURE DISTORTED FLOW FIELD[J].Journal of Aerospace Power,1990,5(1):57-64,92-93. |
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| Authors: | Chen Xiao and Mao Jian |
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| Institution: | Nanjing Aeronautical Institute |
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| Abstract: | A technique of vaying lip simulating total pressure distorted flow field has been investigated experimentally.The effects of the various geometric parameters of the lip on the total pressure distribution and the turbulence of the total pressure fluctuation are analysed,some rules have been obatined.The relations of the total pressure recovery and the mean turbulence to the mean Mach number for the axisymmetrical lip of various shapes are also presented.Therefrom the approach and the concept for simulating the real total pressure distorted flow field are deduced.Moreover,two kinds of the real total pressure distorted flow fields are simulated. |
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