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Numerical and experimental investigation of turbocharger compressor low-end performance improvement using a variable geometry inlet orifice
International Journal of Engine Research ( IF 2.5 ) Pub Date : 2020-08-27 , DOI: 10.1177/1468087420951097 Ben Zhao 1, 2 , Qingjun Zhao 2, 3 , Wei Zhao 2, 3 , Xiaorong Xiang 2, 3 , Xiaoyong Zhou 2, 3
International Journal of Engine Research ( IF 2.5 ) Pub Date : 2020-08-27 , DOI: 10.1177/1468087420951097 Ben Zhao 1, 2 , Qingjun Zhao 2, 3 , Wei Zhao 2, 3 , Xiaorong Xiang 2, 3 , Xiaoyong Zhou 2, 3
Affiliation
Variable geometry orifice located upstream of a centrifugal impeller has been proposed to improve compressor low-end performance, by reducing compressor inlet flow area. The inlet flow area reducti...
中文翻译：
使用可变几何进气孔口的涡轮增压器压气机低端性能改进的数值和实验研究
已经提出位于离心叶轮上游的可变几何孔口，通过减少压缩机入口流动面积来提高压缩机低端性能。进口流通面积减少...
更新日期：2020-08-27
中文翻译：
使用可变几何进气孔口的涡轮增压器压气机低端性能改进的数值和实验研究
已经提出位于离心叶轮上游的可变几何孔口，通过减少压缩机入口流动面积来提高压缩机低端性能。进口流通面积减少...
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