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Parabolized Stability Equations analysis of nonlinear interactions with forced eigenmodes to control subsonic jet instabilities

机译:控制亚声速射流不稳定性的强迫本征模式非线性相互作用的抛物线稳定性方程分析

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摘要

Nonlinear evolution of disturbances in an axisymmetric, high subsonic, high Reynolds number hot jet with forced eigenmodes is studied using the Parabolized Stability Equations (PSE) approach to understand how modes interact with one another. Both frequency and azimuthal harmonic interactions are analyzed by setting up one or two modes at higher initial amplitudes and various phases. While single mode excitation leads to harmonic growth and jet noise amplification, controlling the evolution of a specific mode has been made possible by forcing two modes (m(1), n(1)), (m(2), n(2)), such that the difference in azimuth and in frequency matches the desired " target" mode (m(1) - m(2), n(1) - n(2)). A careful setup of the initial amplitudes and phases of the forced modes, defined as the "killer" modes, has allowed the minimizing of the initially dominant instability in the near pressure field, as well as its estimated radiated noise with a 15 dB loss. Although an increase of the overall sound pressure has been found in the range of azimuth and frequency analyzed, the present paper reveals the possibility to make the initially dominant instability ineffective acoustically using nonlinear interactions with forced eigenmodes. (C) 2015 AIP Publishing LLC.
机译:使用抛物稳定方程(PSE)方法研究了轴对称,高亚音速,高雷诺数热射流具有强迫本征模态下扰动的非线性演化,以了解模态如何相互作用。通过在较高的初始振幅和各个相位设置一个或两个模式,可以分析频率和方位谐波相互作用。虽然单模激励会导致谐波增长和喷射噪声放大,但通过强制两个模式(m(1),n(1)),(m(2),n(2),可以控制特定模式的演变),以使方位角和频率上的差异与所需的“目标”模式(m(1)-m(2),n(1)-n(2))匹配。仔细定义强制模式的初始幅度和相位(定义为“杀手”模式),可以使在近压力场中最初占优势的不稳定性以及其估计的辐射噪声(具有15 dB的损耗)降至最低。尽管已发现在所分析的方位角和频率范围内总声压有所增加,但本论文揭示了使用强制本征模态的非线性相互作用使最初占主导地位的不稳定性在声学上无效的可能性。 (C)2015 AIP Publishing LLC。

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