Erosion wear patterns of turboshaft engine compressor under different radial inlet distortion conditions
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Elsevier BV
Reference39 articles.
1. Multiaxial fatigue damage and reliability assessment of aero-engine compressor blades made of TC4 titanium alloy;Li;Aerosp Sci Technol,2021
2. Solid particle erosion behaviour and protective coatings for gas turbine compressor blades-A review;Alqallaf;Processes,2020
3. Review of damage mechanism and protection of aero-engine blades based on impact properties;Yang;Eng Fail Anal,2022
4. Effects of inlet radial distortion on the type of stall precursor in low-speed axial compressor;Arshad;P I Mech Eng G-J Aer,2018
5. Effect of stress ratio on VHCF behavior for a compressor blade titanium alloy;Huang;Int J Fatigue,2016
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