Effect of cooling hole configurations on combustion and heat transfer in an aero-engine combustor
Authors:
- Huwei DaiHDHuwei Dai
- Junhong ZhangJZJunhong Zhang
- Yanyan RenYRYanyan Ren
- Nuohao LiuNLNuohao Liu
- Jiewei LinJLJiewei Lin
- 1 January 2021
- journal article
- research article
- Published by Elsevier in Applied Thermal Engineering
- Vol. 182
Abstract
No abstract availableKeywords
Funding Information
- National Natural Science Foundation of China (51875397)
- Civil Aviation Administration of China (MRHD20160106)
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