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首页> 外文期刊>International Journal of Aeroacoustics >Nonlinear distortion of traveling waves in non-uniform gasdynamic flows
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Nonlinear distortion of traveling waves in non-uniform gasdynamic flows

机译:非均匀气动力流中行波的非线性畸变

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摘要

A theory of nonlinear wave propagation in quasi-one-dimensional non-uniform gasdynamic flows is developed in order to explain the effect of flow non-uniformity on nonlinear processes such as shock formation and wave quenching. The methodology used is the tracking of the propagating wave front in a hyperbolic system whose evolution is governed by a first order nonlinear ordinary differential equation (Riccati's equation). The present work is an extension of Whitham's wave front expansion method for uniform flow. The equation can be exactly solved for the first derivative of a flow variable at the wave front as a function of the location of wave front in the base flow. This solution is used to develop the criteria for shock formation of a compressive disturbance and quenching of an expansion wave. The solution shows that shock formation depends upon the history of wave propagation. However, quenching of a wave front is independent of the initial slope. The analysis is applied to two important gasdynamic flows: Rayleigh line flow and Fanno line flow. The analysis is a generalization of the authors' previous work in which shock formation in convergent-divergent nozzles was studied (Tyagi and Sujith 2005).
机译:提出了一种在准一维非均匀气动力流中传播非线性波的理论,以解释流动不均匀性对非线性过程(如激波形成和波猝灭)的影响。所使用的方法是在双曲系统中跟踪传播波阵面,该系统的发展由一阶非线性常微分方程(Riccati方程)控制。目前的工作是惠特姆波前扩展方法的扩展,以实现均匀流动。对于波前的流量变量的一阶导数,可以根据基流中波前的位置来精确求解该方程。该解决方案用于制定压缩扰动的冲击形成和膨胀波淬灭的标准。该解决方案表明,冲击的形成取决于波传播的历史。但是,波前的淬灭与初始斜率无关。该分析适用于两个重要的气体动力流:瑞利线流和范诺线流。该分析是作者先前工作的概括,其中研究了会聚-发散喷嘴中的冲击形成(Tyagi和Sujith 2005)。

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