Journal of Thermal Engineering
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Aerothermal Optimization 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 in fluid leakage due to the pressure difference between the pressure side and the
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