Failure Analysis of a Fighter Jet Engine Compressor Blade Due to Foreign Object Damage and High-Cycle Fatigue | SpringerLink
A study of the wear damage on gas turbine blades - ScienceDirect
What could cause a low-pressure compressor first stage blade of a turbofan engine to bend forward? - Aviation Stack Exchange
Fatigue Fracture of a Compressor Blade of an Aeroengine: What Caused this Failure? | SpringerLink
EFFECT OF COMPRESSOR BLADES' OPERATIONAL DAMAGES WITHIN AN AIRCRAFT GAS- TURBINE ENGINE ON ITS PERFORMANCE
Mathematics | Free Full-Text | Effects of Leading-Edge Modification in Damaged Rotor Blades on Aerodynamic Characteristics of High-Pressure Gas Turbine
Compressor blade repair.
5.3.2 Erosion Damage [Aeroengine Safety]
7.1.3 Blade Tip Rubbing Damage [Aeroengine Safety]
Aircraft Turbine Engine Maintenance
Compressor blades damaged by broken vanes of stator (a) and the blade... | Download Scientific Diagram
Turbine Engine Inspection and Maintenance. - TM-1-1500-204-23-1_121
Instances of thermal damages to gas turbine blades: a) – the region of... | Download Scientific Diagram
Housing damage on the compressor blades in a gas turbine power plant [1]. | Download Scientific Diagram
7FA Compressor Blade and Vane Replacement – MDA Turbines
7.1.3 Blade Tip Rubbing Damage [Aeroengine Safety]