Results 71 to 80 of about 161 (89)

Numerical study of effusion cooling of a gas turbine combustor liner

Fuel, 2021
Liang Tian, Jakov Baleta, Jin Wang
exaly  

Effects of lateral cooling hole configuration on a swirl-stabilized combustor

Energy, 2022
Yueliang Zhang, By Dr Jin Xie
exaly  

Numerical investigation on flow and film cooling characteristics of coolant injection in rotating detonation combustor

Aerospace Science and Technology, 2022
Xiao-ming TAN, Jing-zhou Zhang, Jia Tian
exaly  

Analysis of effusion cooling under realistic swirl reacting flow in gas turbine combustor

Applied Thermal Engineering, 2022
Bing Ge, Yongbin Ji, Shusheng Zang
exaly  

Numerical simulations on effect of cooling hole diameter on the outlet temperature distribution for a gas turbine combustor

Applied Thermal Engineering, 2023
Hongtao Zheng
exaly  

Development and performace evaluation of a combustor with silicon carbide microchannel cooling

Experimental Heat Transfer, 2023
Daxiang Deng, Yanlin Xie
exaly  

Effects of wall cooling with microchannels on swirl combustor performance

Aerospace Science and Technology, 2020
Zhiwei Lin, Yue Huang
exaly  

Endwall Film Cooling Performance for a First-Stage Guide Vane With Upstream Combustor Walls and Inlet Injection

Journal of Thermal Science and Engineering Applications, 2019
Zhen-ping Feng, Terrence W Simon
exaly  

Effusion cooling characteristics of a model combustor liner at non-reacting/reacting flow conditions

Applied Thermal Engineering, 2017
Bing Ge, Yongbin Ji, Zhongran Chi
exaly  

Overall cooling effectiveness of effusion cooled annular combustor liner at reacting flow conditions

Applied Thermal Engineering, 2018
Bing Ge, Yongbin Ji, Zhongran Chi
exaly