基于智能优化算法的仿生翼型流控降噪研究

Q3 Engineering
Jingjian Cao, Cui Dai, Junfeng Qiu, Liang Dong
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引用次数: 0

摘要

仿生锯齿结构对中低频气流噪声具有良好的降噪效果,但目前的研究大多集中在有限锯齿数的翼型降噪上,忽略了对锯齿结构参数降噪规律的研究。本文选取齿数、高宽比、钝化比、流切角等4个结构参数,采用数值计算方法研究仿生锯齿翼型的优化设计。提出了一种用于仿生锯齿翼型优化的降噪方法,并找到了降噪效果最佳的锯齿参数。本文以总声压级为优化目标,采用神经网络算法拟合和自适应模拟退火算法进行优化,并通过人工监督的方法对预测结果的合理性进行评价。结果表明,锯齿数对翼型降噪效果的影响最为明显,优化后的总声压级比优化前降低了0.55dB,降噪效果主要集中在翼型后缘附近。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Study on Flow Control and Noise Reduction of Bionic Airfoil Based on Intelligent Optimization Algorithm
The bionic sawtooth structure has a good noise reduction effect on the middle and low frequency flow noise, but the current researches mostly focus on the airfoil noise reduction with limited sawtooth number, ignoring the search for the noise reduction law of the sawtooth structure parameters. In this paper, four structural parameters, including tooth number, height to width ratio, passivation ratio and angle of flow cut, are selected to study the optimization design of bionic sawtooth airfoil by numerical calculation method. A noise reduction method for bionic sawtooth airfoil optimization is proposed, and the sawtooth parameters with the optimal noise reduction effect are found. In this paper, the total sound pressure level is taken as the optimization objective, and the neural network algorithm fitting and adaptive simulated annealing algorithm are employed to optimize, and the rationality of the prediction results is evaluated by the method of manual supervision. The results show that the sawtooth number has the most obvious effect on the airfoil noise reduction effect, and the total sound pressure level after optimization is reduced by 0.55dB compared with that before optimization, and the noise reduction effect is mainly concentrated near the trailing edge of the airfoil.
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来源期刊
International Journal of Fluid Machinery and Systems
International Journal of Fluid Machinery and Systems Engineering-Industrial and Manufacturing Engineering
CiteScore
1.80
自引率
0.00%
发文量
32
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