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汽车空调风道气动噪声仿真方法研究 被引量:14

An Investigation into Simulation Method of Aerodynamic Noise in Vehicle HVAC Ducts
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摘要 为寻求汽车空调风道气动噪声一种高效高精度的仿真方法,基于德国整车企业联合发布的标准风道模型,对比研究了声类比法、直接模拟法和联合仿真分析法的优劣,并重点分析了声源面对声类比法精度的影响。首先,采用RNG湍流模型与SST k-ωDES模型分别对其稳态流场与瞬态流场进行求解,然后采用声类比法、直接模拟法和联合仿真法分别求解远场辐射噪声问题,仿真与试验结果表明:RNG湍流模型捕捉的风道内时均流场特征与PIV测量结果基本吻合; SST k-ωDES模型求解的风道内壁面脉动压力频谱仿真值与试验值基本一致;而在常用的几种仿真方法中,以出风口处环绕射流的可穿透面为声源面的声类比法求解精度最优。 In order to find an efficient and high accuracy simulation method for the aerodynamic noise in vehicle HVAC duets, three commonly-used methods, i.e. acoustic analogy, direct simulation and co-simulation analysis methods are compared and the etchers of sound source surthee on the accuracy of acoustic analogy method are emphatically analyzed, based on the standard HVAC duet model co-issued by German vehicle manufacturers Audi, BMW, Daimler, Porsehe and Volkswagen. Firstly, RNG turbulence model and SST k-ω DES model are adopted to solve the steady state and transient flow fieht respectively. Then, the acoustic analogy, direct simulation and co-sim- ulation methods are used to calculate far fieht radiation noise respectively. The results of simulation and test show that the time-averaged characteristics of tlow-field in HVAC duet obtained with RNG turbulence model are overall agree with PIV measurement data and the fluctuated pressure spectra on duet wall surfaces simulated by SST k-ω DES model are basically consistent with test results. Among commonly-used simulation methods, the acoustic analogy method with the penetrable surrace surrounding the jet turbulence at duet outlet as sound source surface has the highest accuracy.
作者 卿宏军 刘杰 Qing Hongjun;Liu Jie(1.School of Mechanical and Vehicle Engineering,Hunan University,Changsha 410082;CZ-HNU Institute of Machinery Equipment,Changzhou 213164)
出处 《汽车工程》 EI CSCD 北大核心 2018年第11期1370-1375,共6页 Automotive Engineering
基金 国家自然科学基金(11572115)和江苏省创新能力建设计划(BY2015076)资助.
关键词 汽车空调风道 气动噪声 湍流 精度 vehicle HVAC ducts aerodynamic noise turbulence accuracy
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  • 1TAM C K W. Computational aeroacoustics: issues and methods[J]. AIAA, 1995, 33(10) : 1788--1796.
  • 2TAM C K W. Computational aeroacoustics: an overview of computational challenges and applications[J]. International Journal of Computational Fluid Dynamics,2004, 18(6): 547-567.
  • 3TAM C K W, WEBB J C. Dispersion relation preserving finite difference schemes for computational aeousties[J]. Journal of Computational Physics, 1993, 107: 262--281.
  • 4LELE S K. Compact finite difference schemes with spectral-like resolution [J]. Journal of Computational Physics, 1992, 103: 16-42.
  • 5HU F Q,HUSSAINI M Y,MANTHEY J L. Low-dissipation and low-dispersion Runge-Kutta schemes for computational acoustics[J]. Journal of Computational Physics, 1996, 124:177--191.
  • 6STANESCU D, HABASHI W G. 2N-storage low dissipation and dispersion Runge-Kutta schemes for computational acoustics[J]. Journal of Computational Physics, 1998, 143: 674-681.
  • 7CALVO M, FRANCO J M, RANDEZ L. A new minimum storage Runge-Kutta scheme for computational acoustics[J]. Journal of Computational Physics,2004, 201:1--12.
  • 8TSELIOS K, SIMOS T E. Optimized Runge-Kutta methods with minimal dispersion and dissipation for problems arising from computational acoustics[J]. Physics Letters A, 2007, 363: 38--47.
  • 9ALLAMPALLI V, HIXON R, NALLASAMY M,et al. High-accuracy large-step explicit Runge-Kutta ( HALE-RK ) schemes for computational aeroaeousties[J]. Journal of Computational Physics, 2009, 228: 3837--3850.
  • 10RAMBOER J,BROECKHOVEN T, SMIRNOV S, et al. Opti- mization of time integration schemes coupled to spatial diseretization for use in CAA applications[J]. Journal of Computational Physics, 2006, 213: 777-802.

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