Evaluation of Heat Flux by varying Tip Clearance Flow in Axial Compressor Rotor using Thermal Analysis

Abstract

In this Paper analytical investigations are done to determine the effect of unsteady tip clearance flow in axial compressor rotor used in an industrial gas turbine. Thermal analysis is performed by changing the tip clearance 0.333 mm, 0.999 mm and 1.665 mm for different materials Monel K – 500 and Titanium alloy in air as fluid medium. 3D model of axial compressor rotor is drawn in Pro/Engineer and thermal analysis is done in Ansys to obtain total temperature and heat flux for Monel – k 500 and titanium alloy materials using air as a fluid. And Comparative analysis also has done by results of both materials to evaluation of heat flux by varying tip clearance flow in axial compressor rotor using thermal analysis.

Authors and Affiliations

S. Chandana, N. Gopal, P. Srinivasulu, P. Raju

Keywords

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  • EP ID EP22498
  • DOI -
  • Views 210
  • Downloads 4

How To Cite

S. Chandana, N. Gopal, P. Srinivasulu, P. Raju (2016). Evaluation of Heat Flux by varying Tip Clearance Flow in Axial Compressor Rotor using Thermal Analysis. International Journal for Research in Applied Science and Engineering Technology (IJRASET), 4(8), -. https://europub.co.uk/articles/-A-22498