Heat Transfer Characteristics of Pin-Fin Arrays with Ribs to Cool Combustor Liners
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概要
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Enhancement of heat transfer by pin-fin channels with turbulence promoters has been investigated with an aim to improve the cooling efficiency of combustor liners in gas turbines. Time-mean local Nusselt number profiles were obtained by naphthalene sublimation technique based on the heat/mass transfer analogy for Reynolds numbers ranging from 1000-10000. Two oblique rib-type turbulence promoters were tested and compared with no-rib cases. In addition, steady three-dimensional numerical simulations using a RANS model were performed. Installation of turbulence promoters is found to be effective in increasing the endwall heat transfer rate widely and uniformly. In addition, the ribs enhance heat transfer, especially in developing regions at the first and second pin-fin rows. Local high heat transfer regions were obtained in front of the ribs due to horseshoe vortices and downstream of the pins due to a longitudinal vortex.
著者
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Miyake Yoshiaki
Mitsubishi Heavy Industries Ltd.
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Miyake Yoshiaki
Mitsubishi Heavy Industries, Ltd.
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TAKEISHI Kenichiro
Osaka University
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ODA Yutaka
Osaka University
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MOTODA Yusuke
Osaka University
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SUGIMOTO Shinsuke
Osaka University
関連論文
- A213 A Study on the Effect of Angled Pin Fins on Endwall Heat Transfer(Gas Turbine-7)
- Heat Transfer Characteristics of Pin-Fin Arrays with Ribs to Cool Combustor Liners
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