英文期刊论:
国际会议论文:
[9] He Wei, Deng Qinghua*, Yang Guoying, Feng Zhenping. Effects of Turning Angle and Turning Internal Radius on Channel Impingement Cooling for a Novel Internal Cooling Structure. ASME Turbo Expo 2020, Paper No.: GT2020-16115.
[8] He Juan, Deng Qinghua*, Zhou Weilun, He Wei, Gao Tieyu, Feng Zhenping. Conjugate Heat Transfer Characteristics of Double Wall Cooling on a Film Plate with Gradient Thickness. ASME Turbo Expo 2020, Paper No.: GT2020-14275.
[7] He Wei, Deng Qinghua*, He Juan, Gao Tieyu, Feng Zhenping. Heat Transfer and Flow Mechanisms of Jetting Deflection in a Novel Bended Channel Cooling for Gas Turbine Blades. 5th International Workshop on Heat/Mass Transfer Advances for Energy Conservation and Pollution Control, Paper No.: IWHT2019-53.
[6] He Wei, Deng Qinghua*, He Juan, Gao Tieyu, Feng Zhenping. Effects of Jetting Orifice Geometry Parameters and Mach Number on Bended Channel Cooling for a Novel Internal Cooling Structure. ASME Turbo Expo 2019, Paper No.: GT2019-90421.
[5] Zhou Weilun, Deng Qinghua*, He Wei, Feng Zhenping. Effects of Hole Pitch to Diameter Ratio P/D of Impingement and Film Hole on Laminated Cooling Effectiveness. ASME Turbo Expo 2017, Paper No.: GT2017-64566.
[4] Zhou Weilun, Deng Qinghua*, Feng Zhenping. Conjugate Heat Transfer Analysis for Laminated Cooling Effectiveness, Part A: Effects of Surface Curvature. ASME Turbo Expo 2016, Paper No.: GT2016-57243.
[3] Deng Qinghua*, Zhou Weilun, Feng Zhenping. Conjugate Heat Transfer Analysis for Laminated Cooling Effectiveness, Part B: Effects of Film Hole Incline Angle. ASME Turbo Expo 2016, Paper No.: GT2016-57256.
[2] Qi Wenjiao, Deng Qinghua*, Feng Zhenping, Qi Yuan. Influence of Disc Spacing Distance on the Aerodynamic Performance and Flow Field of Tesla Turbines. ASME Turbo Expo 2016, Paper No.: GT2016-57971.
[1] Qi Wenjiao, Deng Qinghua*, Feng Zhenping. Improvement of a Theoretical Analysis Method for Tesla Turbines. ASME Turbo Expo 2013, Paper No.: GT2013-95425.
授权专利:
[7] 邓清华*, 齐文娇, 丰镇平. 一种小型超高速原动机的功率测量装置及方法[P]. 中国发明专利, 专利号201510377068.6. 申请日2015.6.30, 授权公告日2018.2.27.
[6] 邓清华*, 丰镇平. 一种提高向心涡轮性能的叶轮叶片顶部结构[P]. 中国发明专利, 专利号ZL200710019173.8, 申请日2007.11.23, 授权公告日2012.7.25.
[5] 邓清华*, 丰镇平, 李军. 带有隔热与冷却作用的高温燃气密封结构[P]. 中国发明专利, 专利号ZL200410073277.3, 申请日2004.11.15, 授权公告日2007.1.31.
[4] 邓清华*, 蒋宇, 李军, 丰镇平. 超临界二氧化碳布雷顿循环动力部件冷却密封隔热系统. 中国实用新型专利, 专利号ZL201821014675.1, 申请日2018.6.28, 授权公告日2019.3.1.
[3] 邓清华*, 齐文娇, 丰镇平, 袁奇. 盘式透平的轮盘结构[P]. 中国实用新型专利, 专利号ZL201820476182.3, 申请日2018.4.5, 授权公告日2018.9.25.
[2] 邓清华*, 齐文娇, 丰镇平, 袁奇. 盘式透平的喷嘴结构[P]. 中国实用新型专利, 专利号ZL201820477098.3, 申请日2018.4.5, 授权公告日2018.9.25.
[1] 邓清华*, 周玮伦, 丰镇平. 一种三元流离心风机叶轮叶片结构[P]. 中国实用新型专利, 专利号ZL201620139050.X, 申请日2016.2.24, 授权公告日2016.8.10.
国内期刊论文:
[8] 何娟, 邓清华*, 高铁瑜, 丰镇平. 周向角和直径比对切向双旋流冷却流动与传热特性的作用机理. 西安交通大学学报, 2020, 54(10):xxx-xxx.
[7] 邓清华*, 胡乐豪, 石志昊, 丰镇平. 进汽参数对拉伐尔喷管中水蒸气自发凝结的影响研究. 西安交通大学学报, 2020, 54(10): xxx-xxx.
[6] 邓清华*, 胡乐豪, 李军, 丰镇平. 超临界二氧化碳发电技术现状及挑战. 热力透平, 2019, 48(3):159-165.
[5] 邓清华*, 胡乐豪, 李军, 丰镇平. 大型发电技术发展现状及趋势. 热力透平, 2019, 48(3):175-181.
[4] 邓清华*, 颜晓江, 丰镇平. 基于多能互补的分布式能源系统实验教学平台. 实验技术与管理, 2019, 36(5): 215-219.
[3] 邓清华*, 蒋宇, 李军, 丰镇平. 超临界CO2动力循环实验关键技术研究: 循环方案. 热力透平, 2018, 47(2): 93-98+144.
[2] 邓清华*, 蒋宇, 李军, 丰镇平. 超临界CO2动力循环实验关键技术研究: 动力部件. 热力透平, 2018, 47(2): 99-104.
[1] 齐文娇, 邓清华*, 丰镇平, 袁奇. 盘式透平数值方法验证及流动特性分析. 工程热物理学报, 2015, 36(10): 2122-2126.
论著:
[1] 丰镇平, 李祥晟, 邓清华, 徐文文, 谭春青, 高庆, 张前社, 单晓明, 曲丰荣. 《微型燃气轮机应用 安全》. 中华人民共和国国家标准, GB/T38180-2019/ISO 19372:2015, 发布日期: 2019.10.18, 实施日期: 2020.5.1.