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基于全欧拉方程的二维平行剪切层声波产生和辐射的数值模拟
引用本文:李晓东,高军辉.基于全欧拉方程的二维平行剪切层声波产生和辐射的数值模拟[J].航空动力学报,2003,18(2):274-278.
作者姓名:李晓东  高军辉
作者单位:北京航空航天大学能源与动力工程学院,北京100083
基金项目:国家自然科学基金资助项目(10072009)
摘    要:本文基于全欧拉方程对二维平行剪切层声波的产生和辐射进行了计算气动声学数值模拟。空间离散采用了频散相关保持有限差分格式,时间积分采用了低频散低耗散的龙格库塔法。数值模拟结果表明,当声源强度较小时,基于全欧拉方程的计算结果与解析解及基于线化欧拉方程的计算结果均符合得很好,当声源强度较大时(约140dB),线化欧拉与全欧拉的计算结果有较大的偏差,这说明此时非线性的影响不可忽略,线化方程不再适用。 

关 键 词:航空、航天推进系统    计算气动声学    数值模拟    剪切层    不稳定波    高阶格式    无反射边界条件
文章编号:1000-8055(2003)02-0274-05
收稿时间:2002/4/15 0:00:00
修稿时间:2002年4月15日

Numerical Simulation of Sound Generation and Radiation from a 2-D Parallel Shear Layer Based on the Full Euler Equations
Institution:Beijing University of Aeronautics and Astronautics,Beijing100083,China
Abstract:The generation and radiation of acoustic waves from a 2 D shear layer is numerically simulated by an aeroacoustic approach based on the 2 D full Euler equations.The dispersion relation-preserving (DRP) finite difference scheme is employed for space discretization and the low dissipation and low dispersion Runge Kutta (LDDRK) scheme is utilized for time integration.Numerical results show that the full Euler solutions agree well with the analytical solutions as well as the solutions by the linearized Euler equations if the amplitude of sound source is not too large.However,there is great discrepancy between the linear Euler and full Euler solutions if the strength of sound source is strong enough (140 dB).This means that the nonlinear effects can not be neglected whereas the linearized equations do not work.
Keywords:aerospace propulsion  computational aeroacoustics  numerical simulation  shear layer  instability wave  high order schemes  non-reflecting boundary conditions
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