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Heat Transfer Research
Fator do impacto: 0.404 FI de cinco anos: 0.8 SJR: 0.264 SNIP: 0.504 CiteScore™: 0.88

ISSN Imprimir: 1064-2285
ISSN On-line: 2162-6561

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Heat Transfer Research

DOI: 10.1615/HeatTransRes.2016010264
pages 559-574

NUMERICAL INVESTIGATION OF WALL CURVATURE EFFECTS ON HEAT TRANSFER AND FILM COOLING EFFECTIVENESS

A. Shalchi-Tabrizi
Aerospace Engineering Department, Sharif University of Technology, Tehran, I.R. Iran
M. Taiebi-Rahni
Aerospace Engineering Department, Sharif University of Technology, Tehran, I.R. Iran
Gongnan Xie
Department of Mechanical and Power Engineering, Northwestern Polytechnical University, Xi'an, 710072, Shaanxi, China
Masoud Asadi
Department of Mechanical Engineering, Azad Islamic University Science and Research Branch, Tehran, Iran

RESUMO

In this research, the problems of adiabatic film-cooling the flat, convex, and concave surfaces are investigated numerically. Two different radii of curvature and one row of vertical injection holes are considered. The Navier−Stokes equations are solved using a fine nonuniform multiblock staggered curvilinear grid and the SIMPLE-based finite volume method. The blowing rates are 0.5 and 1.0 and the mainstream Reynolds number is 10,000. The obtained results indicated that at a low blowing ratio, the cooling effectiveness enhances over the convex surface and reduces over the concave surface compared to the flat surface case. In comparison with the low blowing ratio, the curvature effects at a high blowing ratio seem to be less pronounced. At the high blowing ratio, the effectiveness is not greatly influenced by the surface curvature.


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