• Anand.R
• S.Karthik
• B.S.Navaneeth

This project deals with the optimization of an axial flow compressor by taking various parameters such as inlet velocity, inlet pressure, blade angle, mean diameter, number of blades and mass flow rate which are taken into the account for increasing the outlet pressure of the compressor blade. By Investigating such required literature modules there parameter are different for achieving outlet pressure from that we done many theoretical calculations by changing the values of those parameters we drawn a graph which contains the varied values of our calculation from that we are concluding our final best optimized design module. And it is drawn using CATIA V5R20 and analyzed it by using ANSYS Fluent software.

CATIA V5R20 ANSYS Fluent software

"Optimization, Design and Analysis of Axial Flow Compressor in Jet Engine", International Journal of Emerging Technologies and Innovative Research (www.jetir.org), ISSN:2349-5162, Vol.6, Issue 6, page no.786-789, June 2019, Available :http://www.jetir.org/papers/JETIR1908A64.pdf

"Optimization, Design and Analysis of Axial Flow Compressor in Jet Engine", International Journal of Emerging Technologies and Innovative Research (www.jetir.org | UGC and issn Approved), ISSN:2349-5162, Vol.6, Issue 6, page no. pp786-789, June 2019, Available at : http://www.jetir.org/papers/JETIR1908A64.pdf