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Publications by M. Y. Jabbari

Film Cooling of the Gas Turbine Endwall by Discrete-Hole Injection

1994English

Related publications

Performance of Gas Turbine Film Cooling With Backward Injection

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Effect of Velocity and Temperature Distribution at the Hole Exit on Film Cooling of Turbine Blades

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The Influences of Off-Design Incidence Angle and Discrete Hole Shapes on Film Cooling Effectiveness

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Effect of Film-Cooling Hole Location on Turbulator Heat Transfer Enhancement in Turbine Blade Internal Air-Cooling Circuits

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Influence of the Pressure Side Injection Slot on the Cooling Performance of Endwall Surface

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Bump and Trench Modifications to Film-Cooling Holes at the Vane-Endwall Junction

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Thermionic Method of Cooling Turbine Blades of Spacecraft Gas Turbine Converters

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