Large-eddy simulation of single-row serrated trenched-hole film cooling on turbine guide vane-Reference-Cited by-同舟云学术

Large-eddy simulation of single-row serrated trenched-hole film cooling on turbine guide vane

Published:2022-04-20 Issue:7-12 Volume:81 Page:119-141
ISSN:1040-7782
Container-title:Numerical Heat Transfer, Part A: Applications
language:en
Short-container-title:Numerical Heat Transfer, Part A: Applications

Author:

Huang Kenan¹,Zhang Jingzhou¹²,Wang Chunhua¹,Liu Song³

Affiliation:

1. College of Energy and Power Engineering, Jiangsu Province Key Laboratory of Aerospace Power System, Nanjing University of Aeronautics and Astronautics, P.R. China

2. Ministry of Industry and Information Technology, Key Laboratory of Thermal Management and Energy Utilization of Aircraft, Nanjing, Jiangsu, P.R. China

3. AECC Sichuan Gas Turbine Research Establishment, Chengdu, P.R. China

Publisher

Informa UK Limited

Subject

Condensed Matter Physics,Numerical Analysis

Link

https://www.tandfonline.com/doi/pdf/10.1080/10407782.2022.2063582

Reference53 articles.

1. Anti-Kidney Pair of Vortices in Shaped Holes and Their Influence on Film Cooling Effectiveness

2. Experimental investigation of jets in a crossflow

3. C. A. Lemmon, A. Kohli, and K. A. Thole, “Formation of counter-rotating vortices in film-cooling flow,” ASME Paper No. 99-GT-161, 1999.

4. Vortical structure in the wake of a transverse jet

5. Numerical investigation on the effects of the divided steps on film cooling performance

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