Influence of non-uniform injection into a transpiration-cooled turbulent channel flow: A numerical study-Reference-Cited by-同舟云学术

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Influence of non-uniform injection into a transpiration-cooled turbulent channel flow: A numerical study

Published:2018-01-07 Issue: Volume: Page:
ISSN:
Container-title:2018 AIAA Aerospace Sciences Meeting
language:
Short-container-title:

Author:

König Valentina¹,Rom Michael¹,Müller Siegfried¹

Affiliation:

1. RWTH Aachen University

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2018-0504

Reference25 articles.

1. Eckert, E., and Livingood, J. “Comparison of Effectiveness of convection- transpiration- and film-cooling methods with air as coolant,” Report 1182, National Advisory Committee for Aeronautics, 1955.

2. Numerical Investigations of Film Cooling

3. Effects of Wall-Temperature Conditions on Effusion Cooling in a Supersonic Boundary Layer

Cited by 3 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Derivation and analysis of a 1D porous medium flow solver embedded in a two-domain model for 2D and 3D transpiration cooling;International Journal of Heat and Mass Transfer;2022-10

2. A Coupled Two-Domain Approach for Transpiration Cooling;Notes on Numerical Fluid Mechanics and Multidisciplinary Design;2020-10-27

3. Effect of gaseous coolant temperature on the transpiration cooling for porous wall in the supersonic flow;International Journal of Heat and Mass Transfer;2019-10

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