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| Study on influence of V-groove on flow field distribution and aerodynamic performance of blunt trailing edge airfoil 期刊论文
Taiyangneng Xuebao/Acta Energiae Solaris Sinica, 2022, 卷号: 43, 期号: 4, 页码: 402-408
作者: Yang, Rui; Gu, Enxin; Zhou, Nannan; Yang, Wei; Wen, Weiyue
  收藏 | 浏览/下载：21/0 | 提交时间：2022/06/20
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| A method for controlled circulation trailing edge design of compressor blade [一种压气机叶型的可控环量尾缘造型方法] 期刊论文
Hangkong Dongli Xuebao/Journal of Aerospace Power, 2019, 卷号: 34, 页码: 142-155
作者:
收藏 | 浏览/下载：6/0 | 提交时间：2019/12/30
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| Combustor wall coolant discharge effects on turbine vane endwall curtain cooling 期刊论文
Journal of Thermophysics and Heat Transfer, 2018, 卷号: 32, 页码: 933-945
作者:
收藏 | 浏览/下载：7/0 | 提交时间：2019/11/19
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| Investigations into film cooling and unsteady flow characteristics in a blade trailing-edge cutback region 期刊论文
Journal of Mechanical Science and Technology, 2018, 卷号: 32, 页码: 5015-5029
作者:
收藏 | 浏览/下载：3/0 | 提交时间：2019/11/26
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| Computation of flow field of a wing with gurney flap in ground effect 会议论文
AIAA Aerospace Sciences Meeting, 2018, 2018-01-08
作者:
收藏 | 浏览/下载：6/0 | 提交时间：2019/12/30
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| Optimization of trailing edge angles of single expansion ramp nozzle based on Kriging method [基于Kriging代理模型的单边膨胀喷管尾缘切角优化] 期刊论文
Hangkong Dongli Xuebao/Journal of Aerospace Power, 2018, 卷号: 33, 页码: 874-881
作者:
收藏 | 浏览/下载：7/0 | 提交时间：2019/12/30
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| Influence of discharge from combustor walls on curtain cooling for a first-stage turbine vane Endwall 会议论文
作者:
收藏 | 浏览/下载：9/0 | 提交时间：2019/11/26
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| Rapid Method to Measure Turbine Blade Based on Laser Sensor 期刊论文
Guangzi Xuebao/Acta Photonica Sinica, 2017, 卷号: 46
作者:
收藏 | 浏览/下载：7/0 | 提交时间：2019/11/26
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| Unsteady Investigations on Cooling Performance of a Gas Turbine Tailing Edge Cut-Back 期刊论文
Hsi-An Chiao Tung Ta Hsueh/Journal of Xi'an Jiaotong University, 2017, 卷号: 51, 页码: 98-103
作者:
收藏 | 浏览/下载：2/0 | 提交时间：2019/11/26
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| Spoiler Upward Deflection on Transonic Buffet Control of Supercritical Airfoil and Wing 期刊论文
JOURNAL OF AIRCRAFT, 2017, 卷号: 54, 页码: 1227-+
作者:
收藏 | 浏览/下载：7/0 | 提交时间：2019/12/30
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