Investigation of the effect of combustor swirl flow on turbine vane full coverage film cooling
Author:
Funder
National Major Science and Technology Projects of China
National Natural Science Foundation of China
Publisher
Elsevier BV
Reference38 articles.
1. Effects of Very high free-Stream turbulence on the jet–mainstream Interaction in a film cooling flow;Kohli,1998
2. Film cooling characteristics of a single round hole at various streamwise angles in a crossflow: Part I effectiveness;Yuen;Int J Heat Mass Tran,2003
3. Influence of the hole length-to-diameter ratio on film cooling with cylindrical holes;Lutum;J Turbomach,1999
4. Study on the film superposition method for dense multirow film Hole layouts;Zhang;Energy,2024
5. Film cooling effectiveness superposition calculation of double-row injection holes on turbine vane;Xu;J Therm Sci,2022
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