Design of a High Pressure Ratio Centrifugal Compressor
نویسندگان
چکیده
منابع مشابه
The Performance of a 6.5 Pressure Ratio Centrifugal Compressor having a Radially-Vaned Impeller
SUMMARY The aerodynamic design and experimental performance of a centrifugal compressor designed for a pressure ratio of 6.5 and a specific speed of 68 are described, The compressor consisted of a radially-vaned impeller and a transonic, vaned radial diffuser. At design speed a peak overall total-to-total isentropic efficiency of 0.746 was achieved at the maximum pressure ratio of 5.9, rising t...
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ژورنال
عنوان ژورنال: DEStech Transactions on Computer Science and Engineering
سال: 2018
ISSN: 2475-8841
DOI: 10.12783/dtcse/cmsam2018/26572