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  Published Paper Details:

  Paper Title

DESIGN OPTIMIZATION OF AN AXIAL FLOW COMPRESSOR USING CFD APPROACH AND EXPERIMENTAL VALIDATION

  Authors

  Mr. Kiran Chaudhari,  Prof. Dr. N. A. Wankhede

  Keywords

Axial flow compressor, aerodynamic design, CFD modeling, experimental validation, wind tunnel cascade test

  Abstract


This paper deals with aerodynamic design of a single stage axial flow compressor for gas turbine engine. The axial flow compressor is designed for the constant tip diameter of the compressor rotor blade for 15.5 kg/s, 14800 RPM, 276.5 KW power with a tip speed 167.7 m/s. The aerodynamic design and blade profiling has been carried out using CFD software. The research starts with design of the high pressure ratio compressor blade sections which yield a single stage pressure rise up to 1.21. Further the design is optimized for minimum total pressure loss. Prototype blade cascades were tested in low speed wind tunnel for performance parameters. Resulting data from experiment s compared with the numerical analysis.

  IJCRT's Publication Details

  Unique Identification Number - IJCRT1705437

  Paper ID - 181539

  Page Number(s) - 1405-1411

  Pubished in - Volume 6 | Issue 1 | January 2018

  DOI (Digital Object Identifier) -    http://doi.one/10.1729/IJCRT.17237

  Publisher Name - IJCRT | www.ijcrt.org | ISSN : 2320-2882

  E-ISSN Number - 2320-2882

  Cite this article

  Mr. Kiran Chaudhari,  Prof. Dr. N. A. Wankhede,   "DESIGN OPTIMIZATION OF AN AXIAL FLOW COMPRESSOR USING CFD APPROACH AND EXPERIMENTAL VALIDATION", International Journal of Creative Research Thoughts (IJCRT), ISSN:2320-2882, Volume.6, Issue 1, pp.1405-1411, January 2018, Available at :http://www.ijcrt.org/papers/IJCRT1705437.pdf

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ISSN: 2320-2882
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Journal Starting Year (ESTD) : 2013
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ISSN and 7.97 Impact Factor Details


ISSN
ISSN
ISSN: 2320-2882
Impact Factor: 7.97 and ISSN APPROVED
Journal Starting Year (ESTD) : 2013
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