Design of Multi-Stage Axial Flow Compressor and Validation using Numerical Simulations
Cheke K. D.*,
Kamble A.G.
Abstract:The optimum yield of gas turbine engines has so far been driven on and around the operational efficiency of the compressor and in essence around the efficiency of the compressor blade. The efficacy of a compressor is ascertained substantially by the smoothness of the air flowing through it. In this present work, a multi-stage axial compressor in the Turbojet engine with an application for propulsion is designed based on thermodynamic calculations. The calculations were carried out employing the principles of t… Show more
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