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连续式跨声速风洞轴流压缩机气动设计与低噪声设计
引用本文:龙炳祥,刘宗政,陈振华,陈吉明,雷鹏飞.连续式跨声速风洞轴流压缩机气动设计与低噪声设计[J].实验流体力学,2022,36(1):27-36.
作者姓名:龙炳祥  刘宗政  陈振华  陈吉明  雷鹏飞
作者单位:中国空气动力研究与发展中心 设备设计与测试技术研究所,绵阳 621000
摘    要:连续式跨声速风洞是采用轴流压缩机驱动的、可持续运行的变密度回流式风洞.一方面,此类风洞具有运行工况范围宽的典型特征,驱动风洞主回路气流的轴流压缩机需要具备在宽工况范围稳定高效运行的能力;另一方面,良好的风洞试验段动态流场品质要求轴流压缩机进出口气流噪声不高于140 dB.宽工况范围的高效稳定运行要求和低噪声设计要求给连...

关 键 词:风洞  轴流压缩机  气动设计  低噪声设计
收稿时间:2021-08-02

Aerodynamic and aero-acoustic design of continuous transonic wind tunnel compressor
Institution:Facility Design and Instrumentation Institute of China Aerodynamics Research and Development Center, Mianyang 621000, China
Abstract:The continuous transonic wind tunnel, which is generally a closed-circuit variable-density wind tunnel, is an excellent platform for aerodynamic mechanism research and advanced aero vehicles development. A cost-effective and stable continuous transonic wind tunnel requires its driver, usually a multistage axial-flow compressor, to have wide operating range with high adiabatic efficiency and sufficient surge margin. On the other hand, the good test section flow quality requires the outlet and inlet aero-acoustic noise of the compressor lower than 140 dB. Developing a multi-stage axial-flow compressor with high adiabatic efficiency, sufficient surge margin and low noise level working under extra-wide operating conditions faces many challenges. Thus, the effectiveness of the variable geometry method, including variable rotor blade and variable stator vanes, the choice of design point and its corresponding load coefficient and flow coefficient, and the choice of meridional type and the basic principles related to low-noise axial-flow compressor design, were analyzed for the purpose of providing some guidance for designing such a compressor. For compressors with the reaction degree higher than 0.5, the variable rotor blade is more effective. For compressors with the reaction degree lower than 0.5, the variable stator vanes method is more effective than variable rotor blade method. For wind tunnels with operating range from Ma=0.2–1.6, the design point of the compressor should be around Ma=1.4 and its corresponding loading coefficient and flow coefficient are about 0.6 and 0.25 respectively. The constant tip radius meridional type has advantages in aerodynamic performance improvement. Larger rotor-stator spacing and appropriate rotor/stator number ratio are effective in suppressing the compressor noise emission.
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