Results 11 to 20 of about 71,914 (314)
The Combined Influences of Film Cooling and Thermal Barrier Coatings on the Cooling Performances of a Film and Internal Cooled Vane [PDF]
This paper presents a numerical investigation on the combined influences of film cooling and thermal barrier coatings (TBCs) on the cooling performances of a NASA C3X guide vane. The results show that: (1) film cooling on the pressure side is more effective than suction side, especially on the trailing edge where multiple cooling and thermal protection
Li Shi, Zhiying Sun, Yuanfeng Lu
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In present study, the heat transfer and the throughflow losses characteristics of single/triple-row of fan-shaped and cylindrical film cooling holes with a fixed outlet width are studied experimentally with an engine-representative density ratio.
H. Wei, Y.Q. Zu
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Experimental investigations have been conducted to improve the cooling effectiveness of film-cooling technology. A multiple row of cylindrical holes at the flat surface was considered by inclining the holes at 35° along the streamwise direction.
Jaemun Choi +5 more
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Local Heat Transfer Measurements on a Rotating Flat Blade Model with a Single Film Hole [PDF]
An experimental study was performed to measure the heat transfer coefficient distributions on a flat blade model under rotating operating conditions. A steady-state thermochromic liquid crystal technique was employed to measure the surface temperature ...
Tao, Zhi +8 more
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Film-cooling hole optimization and experimental validation considering the lateral pressure gradient
The flow in the turbine endwall region consists of the complicated secondary flow structures driven by the lateral pressure gradient, which heavily affects the performance of film cooling.
Hao Zhang +4 more
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Uncertainty quantification and film cooling
zbMATH Open Web Interface contents unavailable due to conflicting licenses.
D'Ammaro, A, Montomoli, F
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In this paper, the effects of internal coolant crossflow on double-jet holes were simulated and compared with two rows of cylindrical holes under three blowing ratios (M = 0.5, 1.0, and 1.5), with an established and validated turbulence model.
Xie, Gongnan, +4 more
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Evaluation of film cooling channel geometries in gas turbine blades [PDF]
ilustraciones, diagramasLa refrigeración por película ha permitido incrementar las temperaturas de trabajo en álabes de turbinas de gas, al mantener parte de la superficie cubierta por un flujo de refrigerante de menor temperatura que el flujo ...
Pinzón Rincón, Christian David
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Study on the effect of waveform film holes on film cooling efficiency
In order to improve the film cooling efficiency of the cooling gas on the hot side wall of the plate, the flow field, temperature field and the average film cooling efficiency of the cylindrical hole, rectangular hole and waveform hole near the wall were
Cheng Qian +4 more
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Effects of Turbulence Promoters of Gas Turbine Blades on Film Cooling Performance
The effects of orientation of turbulence promoting ribs in the internal cooling air passage on the film cooling performance of outer surface of gas turbine blades have been studied experimentally.
Yukiko AGATA +3 more
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