Identification of noise source is of important significance for noise control. In this paper, a multiple input/ single output model for system noise identification is established. The technique of measurement of noise source contribution and partial coherence analysis are introduced and discussed. The formula of partial coherence function is given by "residual spectrum". Aiming at 0.55m × 0.4m aeroacoustic wind tunnel, the measurement scheme is presented. According to the noise measurement data, the main noise source in aeroacoustic wind tunnel is identified.%噪声源识别对噪声控制具有重要意义.在建立多输入/单输出系统噪声模型,分析介绍噪声源贡献量测量及偏相干分析技术的基础上,给出偏相干函数的条件谱计算公式.针对0.55 m×0.4 m航空声学风洞,拟定噪声测试方案.结合噪声测试数据,表明风洞主要噪声源识别的有效性.
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