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Analysis of Low-Pressure Turbine Nozzle Guide Vane Failure in an Aero Gas Turbine Engine: A Computational Approach
Authors:Kumaresan  D. Arul  Mishra   R. K.
Affiliation:1.Regional Centre for Military Airworthiness (Engines), CEMILAC, Bangalore, 560093, India
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Abstract:Journal of Failure Analysis and Prevention - Failure of low-pressure turbine nozzle guide vane (NGV) in an aero gas turbine engine is analyzed using computational approach. Breakage in the cooling...
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