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Failure Analysis of a Fighter Jet Engine Compressor Blade Due to Foreign Object Damage and High-Cycle Fatigue | SpringerLink
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Why isn't aluminium used in the compressor section of a jet engine? Heat is not a factor, so why use costly titanium? - Quora
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Detail of the compressor blades on a General Electric CF6 jet engine [3120x4160] [OC] : r/MachinePorn
Compressor blades damaged by broken vanes of stator (a) and the blade... | Download Scientific Diagram
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