Results 21 to 30 of about 1,878,968 (293)
Modern gas turbines have evolved by increasing the turbine inlet temperature (TIT) to improve performance. This development has led to a demand for cooling techniques.
Seokmin Kim +3 more
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Uncertainty quantification and film cooling
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D'Ammaro, A, Montomoli, F
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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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Numerical Study on Film-Cooling Effectiveness for Various Film-Cooling Hole Schemes
Film-cooling has been widely used as the important alternative to protect the turbine blade. Since the film-cooling hole geometry is one of the most influential parameters for film-cooling performance, various film-cooling hole schemes have been developed to increase cooling performance for the past few decades.
S.M. Kim, K.D. Lee, K.Y. Kim
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Film cooling modeling of a turbine vane with multiple configurations of holes
Film cooling flow is important for gas turbine thermal protection. But it is difficult to predict the film cooling flow performances. The aim of this paper is to modeling the film cooling flow of a turbine vane with endwall film cooling, showerhead film ...
J.H. Liu, Y.B. Liu, L. Liu
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Cooling Characteristics of Film-Cooled Turbine Blades [PDF]
A series of experiments was performed to measure the cooling effectiveness of pin-fin type blades applicable to the first-stage blades of the high pressure turbine for the Advanced Gas Turbine of Japan (AGTJ-100A). Actual pin-fin type blades were used in three-dimensional hot cascade tests.
T. Abe +5 more
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Effect of an Upstream Unconnected Bulge on Film Cooling
Film cooling technology is commonly used in a cooling system of gas turbines. For different upstream bulge configurations, the unconnected and connected configurations were used to investigate the film cooling effectiveness and downstream dimensionless ...
Q. Li +5 more
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Experimental study on a spray and falling-film cooling system
After spraying, the cooling medium retains potential cooling capability and, consequently, can form a falling film to further cool the downward area. In this paper, the flow patterns and the heat transfer coefficients are correlated respectively in the ...
Yuqi Huang +3 more
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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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Investigation on the Effect of Impingement Chamber Structure and Cooling Unit Number on Composite Cooling [PDF]
In order to deeply explore the influence and mechanism of the impingement chamber structure and the number of cooling units on the film cooling performance.
J. Liu, Z. Zhu, J. Chang, S. Ma, J. Sun
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