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Aerothermal optimizaiton of squealer geometry in axial flow turbines using genetic algorithm
In turbomachines, a tip gap is required in order to allow the relative motion of the blade and to prevent the blade tip surface from rubbing. This gap which lay out between the blade tip surface and the casing, results ... -
A genetic algorithm based multi-objective optimization of squealer tip geometry in axial flow turbines: A constant tip gap approach
Maral, Hıdır; Şenel, Cem Berk; Deveci, Kaan; Alpman, Emre; Kavurmacıoğlu, Levent Ali; Camci, Cengiz (2020)Tip clearance is a crucial aspect of turbomachines in terms of aerodynamic and thermal performance. A gap between the blade tip surface and the stationary casing must be maintained to allow the relative motion of the blade. ...
