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- [43] Failure Analysis on Foreign Object Damage of Aero-engine Compressor Blade PROCEEDINGS OF 2009 8TH INTERNATIONAL CONFERENCE ON RELIABILITY, MAINTAINABILITY AND SAFETY, VOLS I AND II: HIGHLY RELIABLE, EASY TO MAINTAIN AND READY TO SUPPORT, 2009, : 1085 - 1088
- [44] THE EFFECT OF ADDITIVE 'DEPOSITIONAL' REPROFILING OF COMPRESSOR BLADE LEADING EDGES ON ENGINE PERFORMANCE PROCEEDINGS OF ASME TURBO EXPO 2024: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, GT2024, VOL 12B, 2024,
- [45] Gas Turbine Aero Engine Compressor Blade Erosion and Heat Resistant Coatings TRANSPORT MEANS 2011, 2011, : 274 - 278
- [46] Thermal Contact Resistance between Aero Engine Compressor Blade and Flexible Fixture Journal of Thermal Science, 2021, 30 : 530 - 539
- [48] Comparative Analysis of Gas-Turbine Engine Compressor Blade Survivability. Problemy Prochnosti, 1981, (08):
- [49] PREDICTION OF GAS TURBINE ENGINE COMPRESSOR ROTOR BLADE SERVICE LIFE. Soviet Aeronautics (English translation of Izvestiya VUZ, Aviatsionnaya Tekhnika), 1973, 16 (04): : 100 - 103
- [50] Investigation of laser shock peening on aero-engine compressor rotor blade SURFACE ENGINEERING (ICSE 2007), 2008, 373-374 : 404 - 407