International Journal of Scientific and Research Publications

IJSRP, Volume 8, Issue 9, September 2018 Edition [ISSN 2250-3153]


Five-Stage Axial Flow Compressor for Gas Turbine
      Khema Theint
Abstract: The goal of this paper is to calculate the blade design of axial flow compressor. Main objective of the compressor usage is to compress the fluid and to deliver higher pressure than its original pressure. So, the stagnation pressure ratio and overall pressure ratio are calculated in this paper. Blade mean diameter is 0.295 m for all five stages.

Reference this Research Paper (copy & paste below code):

Khema Theint (2018); Five-Stage Axial Flow Compressor for Gas Turbine; International Journal of Scientific and Research Publications (IJSRP) 8(9) (ISSN: 2250-3153), DOI: http://dx.doi.org/10.29322/IJSRP.8.9.2018.p8129
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