Investigation of Stress Intensity Factor of Axial Compressor Blade of Helicopter

An article published in the « International Journal of Ethics in Engineering & Management Education » of july 2015.

Compress blade fails under several factors like high cycle fatigue, due to high rotational velocity, corrosiveness area, due to impinging foreign particle on compressor blade and also hard landing. This paper presents the failure analysis of compressor blade of helicopter engine.

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