TS-50 Heat Transfer Enhancements on Combustor Liner with Impingement/Effusion Cooling(Session C-2 Heat Transfer 2)

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概要

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• The present study is conducted to investigate the local heat/mass transfer characteristics for flow through perforated plates. A naphthalene sublimation method is employed to determine the local heat/mass transfer coefficients on the effusion plate. Two parallel perforated plates are arranged for the two different ways: staggered and shifted in one direction. The experiments are conducted for hole pitch-to-diameter ratios of 6.0, for gap distance between the perforated plates of 0.33 to 10 hole diameters, and for Reynolds numbers of 5,000 to 12,000. The result shows that the high transfer region is formed at stagnation region and at the midline of the adjacent impinging jets due to secondary vortices and flow acceleration to the effusion hole. For flows through the perforated plates, the mass transfer rates on the surface of the effusion plate are about six to ten times higher than for effusion cooling alone (single perforated plate). More uniform and higher heat/mass transfer characteristic is obtained in overall region with small gap between two perforated plates.

• 社団法人日本ガスタービン学会の論文
• 1999-11-14

著者

• Cho H.h.

  Department Of Mechanical Engineering Yonsei University

• RHEE D.H.

  Department of mechanical engineering, Yonsei University

• Rhee D.h.

  Department Of Mechanical Engineering Yonsei University

関連論文

• TS-50 Heat Transfer Enhancements on Combustor Liner with Impingement/Effusion Cooling(Session C-2 Heat Transfer 2)

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