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- W2184175089 abstract "The ingestion of foreign objects into aircraft jet engines can lead to severe structural damage of the fan and/or compressor blades. The foreign object damage (FOD) is a prime reason for maintenance and repair of jet engines. The damage induced by small hard objects of millimeter size in conjunction with the typical load spectra experienced by airfoils can lead to non-conservative life prediction and unexpected fatigue failures. The worst conditions are experienced during takeoff which leads to maximum thrust that in turn leads to maximum impact velocity. Typical impact velocities are in the range of 100 - 400 m/s, depending on the type of engine. As per the stipulated standards the maximum allowable value of stress concentration for the compressor aerofoil is limited to 3. Due to complex shape and geometry of the aerofoil there exist no closed form solutions for the typical compressor aerofoil. Hence finite element analysis is carried out to obtain the stress concentration factor values for semicircular notches by varying the location and radius on rectangular plate in rotation and the results obtained are compared by carrying out the analysis on the typical aerofoil." @default.
- W2184175089 created "2016-06-24" @default.
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- W2184175089 date "2014-01-01" @default.
- W2184175089 modified "2023-09-27" @default.
- W2184175089 title "Stress Concentration Factor Analysis with Semicircular cut outs on FO damaged Compressor Blade of Aero Engine a Parametric Approach" @default.
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