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Submit your paper : editorIJETjournal@gmail.com ![]() ISSN : 2395-1303 Year of Publication : 2021 ![]() ![]() ![]() MLA Style: -Dr Srikanth Salyan,Dhanesh Gavimath,Dhanush S D,Ganti Akshay,Sanjay Kumar H M , " Performance analysis of centrifugal compressor with variable diffuser " Volume 7 - Issue 4 July - August,2021 International Journal of Engineering and Techniques (IJET) ,ISSN:2395-1303 , www.ijetjournal.org APA Style: -Dr Srikanth Salyan,Dhanesh Gavimath,Dhanush S D,Ganti Akshay,Sanjay Kumar H M, " Performance analysis of centrifugal compressor with variable diffuser " Volume 7 - Issue 4 July - August,2021 International Journal of Engineering and Techniques (IJET) ,ISSN:2395-1303 , www.ijetjournal.org Abstract - This paper includes design and analysis of centrifugal compressors with variable diffuser. The main agenda of this work is to investigate the effects of centrifugal compressors with variable diffuser on mass flow rate, pressure ratio and performance of a compressor, and to optimize the design to get better performances. A standard centrifugal compressor was designed as per the design specifications of NASA’s low speed centrifugal compressor with diffusers having different vanes angles from -6 to +6 degrees. After the performance analysis, we came to know that when a compressor is getting inadequate amount of mass flow rate that can cause surging of the compressor, by increase of diffuser vane angle we can shift the surge point to the lower values so that the mass flow which a compressor is getting could come under operating condition. The negative diffuser angles are benefitting when a compressor gets adequate amount of mass flow as they increase the efficiencies. Reference 1. EthirajanRathakrishnan. (2010, pp. 59-63). “Gas Dynamics” (3rd Ed.). New Delhi-110001, India: Ashok K Ghosh, PHI Learning Private Ltd. 2. Ahmed F. El-Sayed. (2008, pp. 551-605). “Aircraft Propulsion and Gas Turbine Engines”. Taylor and Francis Group, 6000 Broken Sound Parkway NW, Suite 300, Boca Raton, FL 33487-2742: CRC Press. 3. Mohsen Ebrahimi, Qiangqiang Huang, Xiao He and Xinqian Zheng (12 May 2017) Article “Effects of Variable Diffuser Vanes on Performance of a Centrifugal Compressor with Pressure Ratio of 8.0”. Tsinghua University, Beijing 100084, China. 4. Kuo-Shu Hung1, Jenn-Chyi Chung1, Chung-Che Liu1 and Jeng-Min Huang2’(2017) Research Article “A study of off-design performance improvement for a centrifugal refrigerant compressor”(Vol. 9(3) 1–10). 5. Mohammad javad Hosseini, Zhenzhong Sun, Xiao He and Xinqian Zheng. (2017). Article “Effects of Radial Gap Ratio between Impeller and Vaned Diffuser on Performance of Centrifugal Compressors”. Beijing 100084, turbomachinery laboratory. 6. KangsooIm’s Dissertation (2012) “Development of a Design method for Centrifugal Compressors”. Michigan State University. 7. M. D. Hathaway, et al. (1991). “NASA Low-Speed Centrifugal Compressor for 3-D Viscous Code Assessment and Fundamental Flow Physics Research”. 36th International Gas Turbine and Aero engine Congress and Exposition sponsored by American Society of Mechanical Engineers Oelando, Florida. 8. Y. B. Galerkin, et al. (2017). “Comparison of CFDcalculations of centrifugal compressor stages by NUMECA Fine Turbo and ANSYS CFX programs”. St Petersburg Polytechnic University, Russia Keywords —— |