Effect of Spanwise Hole-to-Hole Spacing on Overall Cooling Effectiveness of Effusion Cooled Combustor Liners for a Swirl-Stabilized Can Combustor

被引:0
|
作者
Ahmed, Shoaib [1 ]
Wahls, Benjamin H. [2 ]
Ekkad, Srinath V. [3 ]
Lee, Hanjie [4 ]
Ho, Yin-Hsiang [5 ]
机构
[1] Mechanical and Aerospace Engineering, North Carolina State University, 911 Oval Drive, Engineering Building III, Room 3002, Raleigh,NC,27695, United States
[2] Mechanical and Aerospace Engineering, North Carolina State University, 1840 Entrepreneur Drive, Room 3002, EB3, Raleigh,NC,27695, United States
[3] Mechanical and Aerospace Engineering, North Carolina State University, 911 Oval Drive, 3002 EB III, Raleigh,NC,27695, United States
[4] Solar Turbines Inc., 2200 Pacific Highway, P. O. Box 85376, Combustion Engineering, San Diego,CA,85376, United States
[5] Solar Turbines Inc., 2200 Pacific Highway, P. O. Box 85376, Mail Zone E-4 Combustion Engineering, San Diego,CA,85376, United States
来源
Journal of Turbomachinery | 2022年 / 144卷 / 07期
关键词
26;
D O I
暂无
中图分类号
学科分类号
摘要
引用
收藏
相关论文
共 17 条
  • [1] Effect of Spanwise Hole-to-Hole Spacing on Overall Cooling Effectiveness of Effusion Cooled Combustor Liners for a Swirl-Stabilized Can Combustor
    Ahmed, Shoaib
    Wahls, Benjamin H.
    Ekkad, Srinath V.
    Lee, Hanjie
    Ho, Yin-Hsiang
    [J]. JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2022, 144 (07):
  • [2] Effect of Spanwise Hole to Hole Spacing on Overall Cooling Effectiveness of Effusion Cooled Combustor Liners for a Swirl Stabilized Can Combustor
    Ahmed, Shoaib
    Wahls, Benjamin H.
    Ekkad, Srinath
    Lee, Hanjie
    Ho, Yin-Hsiang
    [J]. PROCEEDINGS OF ASME TURBO EXPO 2021: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, VOL 5A, 2021,
  • [3] EXPERIMENTAL STUDY ON OVERALL COOLING EFFECTIVENESS OF SWIRL-STABILIZED MODEL COMBUSTOR WITH EFFUSION COOLING
    Ji, Yongbin
    Zhang, Liang
    Jin, Ming
    Ge, Bing
    Zang, Shusheng
    Xin, Jianhua
    Wu, Weiliang
    Li, Mingjia
    Xu, Wenyan
    [J]. PROCEEDINGS OF THE ASME TURBO EXPO: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, 2019, VOL 5A, 2019,
  • [4] Comparison of effusion cooling characteristics between different hole configurations in a swirl-stabilized combustor
    Lu, Xiang
    Jia, Yuliang
    Ji, Yongbin
    Ge, Bing
    Zang, Shusheng
    [J]. Hangkong Dongli Xuebao/Journal of Aerospace Power, 2024, 39 (12):
  • [5] Effects of lateral cooling hole configuration on a swirl-stabilized combustor
    Zhang, Yueliang
    Li, Jiangheng
    Xie, Jin
    [J]. ENERGY, 2022, 259
  • [6] EFFUSION COOLING CHARACTERISTICS OF EFFUSION-COOLED COMBUSTOR LINERS WITH DIFFERENT HOLE CONFIGURATIONS UNDER SWIRL IMPACT
    Lu, Xiang
    Jia, Yuliang
    Ji, Yongbin
    Ge, Bing
    Zang, Shusheng
    [J]. PROCEEDINGS OF ASME TURBO EXPO 2024: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, GT2024, VOL 7, 2024,
  • [7] Effect of the hole configurations on effusion cooling effectiveness under swirl impact in gas turbine combustor
    Lu, Xiang
    Jia, Yuliang
    Ji, Yongbin
    Ge, Bing
    Zang, Shusheng
    [J]. INTERNATIONAL JOURNAL OF THERMAL SCIENCES, 2024, 203
  • [8] Overall Cooling Effectiveness of Effusion Cooled and Thermal Barrier Coated Swirl Stabilized Liquid Fueled Combustor Liner in Reacting Flow Conditions
    Ozogul, Hamdullah
    Tin, Ibrahim Edhem
    [J]. PROCEEDINGS OF ASME TURBO EXPO 2023: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, GT2023, VOL 7A, 2023,
  • [9] Overall cooling effectiveness of effusion cooled annular combustor liner at reacting flow conditions
    Ji, Yongbin
    Ge, Bing
    Chi, Zhongran
    Zang, Shusheng
    [J]. APPLIED THERMAL ENGINEERING, 2018, 130 : 877 - 888
  • [10] Overall Cooling Effectiveness of Effusion Cooled Can Combustor Liner under Reacting and Non-Reacting Conditions
    Ahmed, Shoaib
    Ramakrishnan, Kishore Ranganath
    Ekkad, Srinath
    Singh, Prashant
    Liberatore, Federico
    Ho, Yin-Hsiang
    [J]. PROCEEDINGS OF THE ASME TURBO EXPO: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, VOL 7A, 2020,