Effusion cooling plates for combustor liners: experimental and numerical investigations on the effect of density ratio

被引:28
|
作者
Andrei, Luca [1 ]
Andreini, Antonio [1 ]
Bianchini, Cosimo [1 ]
Caciolli, Gianluca [1 ]
Facchini, Bruno [1 ]
Mazzei, Lorenzo [1 ]
Picchi, Alessio [1 ]
Turrini, Fabio [2 ]
机构
[1] Univ Florence, Dept Ind Engn, Via Santa Marta 3, I-50139 Florence, Italy
[2] Avio Aero, Combust Syst Off, Turin I-10040, Italy
关键词
effusion cooling; adiabatic effectiveness; algebraic anisotropic correction; turbulence modeling; PSP technique; TURBINE-BLADES; FILM; FLOW;
D O I
10.1016/j.egypro.2014.01.147
中图分类号
O414.1 [热力学];
学科分类号
摘要
Effusion cooling represents the state-of-the-art of liner cooling technology for modern combustors. The present paper describes experimental tests aiming at evaluating the cooling performance of a multi-perforated plate in real engine representative fluid-dynamic conditions. Adiabatic effectiveness maps were obtained following the mass transfer analogy by the use of Pressure Sensitive Paint. In addition, a CFD campaign was performed in order to benchmark the reliability in estimating the cooling performance of effusion cooling liners. In order to include anisotropic diffusion effects, the k - omega SST turbulence model was corrected considering a tensorial definition of the eddy viscosity with an algebraic correction to dope its stream-span components. (C) 2013 The Authors. Published by Elsevier Open access under CC BY-NC-ND license.
引用
收藏
页码:1402 / 1411
页数:10
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