Inductive Plasma Excitation Forcing Configuration on Reduction of Tip Distorted Inflow Effect on the Aerodynamic Stability of Axial Compressor Rotor

Author:

Khoshnejad Ali,Ebrahimi Reza,Pouryoussefi Sohrab Gholamhosein

Publisher

Elsevier BV

Reference45 articles.

1. Experimental investigation of a high aspect ratio, low speed contra-rotating fan stage with complex inflow distortion;Mistry;Propulsion and Power Research,2014

2. Influence of inlet distortion on the wear of aero-compressor blades;Li;International Journal of Mechanical Sciences,2022

3. Effect of swirl distortion on gas turbine operability;Mehdi,2014

4. The effect of inlet distortion on low bypass ratio turbofan engines;Verma;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering,2020

5. Experimental investigation and detached-eddy simulation of compressor aerodynamic performance in inlet distortion;Zhou;AIP Advances,2019

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