Blank1

 主持完成及在研的项目：

纵向课题：

2021.01-2024.12，国家自然科学基金面上项目——燃气透平高温叶片前缘旋流/气膜复合冷却气热性能与流热耦合机理研究；

2021.01-2025.12    重大专项——透平密封、腔室、榫头/榫槽流动传热及冷却研究；

2018.08-2023.07    重大专项——燃气透平动叶叶顶流动传热及冷却研究；

2015.01-2017.12，国家自然科学基金青年基金项目——叶片前缘旋流冷却研究；

2014.01-2016.12，高等学校博士学科点专项科研基金——燃气透平端壁传热冷却研究；

2013.06-2014.05，陕西省自然科学基金青年类项目——端壁冲击/气膜复合冷却研究；

2013.06-2014.05，博士后基金项目——叶片前缘冲击/气膜复合冷却研究

横向课题：

2019.10-2020.12，校企合作项目——叶栅气膜冷却优化及试验验证；

2018.08-2019.06，校企合作项目——燃气透平叶栅气膜冷却试验；

 

参与的项目：

2020.01-2023.12，国家自然科学基金面上项目——太阳能驱动的超临界CO2布雷顿循环发电系统能量匹配机理与全域调控方法研究；

2018.10-2019.12，校企合作项目——高压涡轮流热耦合分析及叶顶冷却设计优化；

2014.01-2018.12，国家自然科学基金重点项目——考虑热斑和冷气掺混的多级燃气透平非定常流动与传热机理研究；

2013.7-2016.6，校企合作项目——叶片端壁冷却技术研究；

2012.8-2014.12，校企合作项目——工业燃气轮机透平第一级静叶流动及冷却特性研究；

 

杭汽横向课题——工业汽轮机末三级通流优化；

973项目课题1项；

企业横向课题3项；

Blank

 

2023年：

  1. Feng Li, Weixin Zhang, Zhao Liu*, Zhenping Feng. Heat Transfer Measurements of the Multi-cavity Tips with Different Turbulence Levels. Journal of Heat Transfer-Transactions of the ASME. Accepted manuscript posted November 14, 2022. doi:10.1115/1.4056228.
  2. 刘钊, 张韦馨, 谢晔航, 丁玉强, 丰镇平. 装配间隙泄漏流对透平端壁冷却影响的实验研究. 西安交通大学学报, 2023, 57(04), pp. 1-11.
  3. Weixin Zhang, Feng Li, Yehang Xie, Yuqiang Ding, Zhao Liu, Zhenping Feng, Experimental and numerical investigations of discrete film holes cooling performance on a blade endwall with mid-passage gap leakage, International Journal of Heat and Mass Transfer, Volume 201, Part 1, 2023, 123550, ISSN 0017-9310, https://doi.org/10.1016/j.ijheatmasstransfer.2022.123550. (SCI)

​​​​​​​

2022年：

  1. 刘钊, 谢晔航, 张韦馨, 丰镇平, 一种模拟涡轮动静盘腔泄漏流预旋的试验结构, 发明专利，2022.10.28 (专利号：ZL202210028951.4)
  2. 刘钊, 李冯, 贾哲, 王海锋, 张韦馨, 丰镇平, 一种用于测量透平动叶叶顶换热系数的实验系统和稳态实验方法, 发明专利，2022.08.05 (专利号：ZL 2021 1 1159130.6)
  3. 刘钊, 王海锋, 张韦馨, 李冯, 贾哲, 谢晔航, 丰镇平, 一种测量叶栅气膜冷却特性的试验系统, 发明专利，2022.06.07 (专利号：ZL 2021 1 1077874.3
  4. 刘钊, 张韦馨, 刘战胜, 杨星, 丰镇平,一种端壁气膜孔布置结构, 发明专利，2021.05.28 (专利号：ZL202010611065.5)
  5. 李冯, 贾哲, 张韦馨, 刘钊*, 石龑, 丰镇平, 透平动叶多凹槽叶顶气膜冷却特性的研究. 西安交通大学学报, 2022, 56(08), pp. 1-12. DOI: 10.7652/xjtuxb202208016. (EI, 20223812763898)
  6. Feng Li, Zhe Jia, Haifeng Wang, Zhao Liu*, Zhenping Feng, Investigation into the Film Cooling Performance of Multi-Cavity Tips with Different Cavity Depths. International Journal of Thermal Science,2022, 181, p.107766. DOI: 10.1016/j.ijthermalsci.2022.107766. (WOS:000825092800003)
  7. Feng Li, Weixin Zhang, Zhe Jia, Zhao Liu*, Zhenping Feng, Experimental Study about the Tip Phantom Cooling with Different Cooling-Hole Configurations on the Blade-Surface. International Journal of Heat and Mass Transfer, 2022, 194, p. 122999. DOI: 10.1016/j.ijheatmasstransfer.2022.122999. (WOS:000806815900008), 5.431, Q1
  8. Feng Li, Zhe Jia, Haifeng Wang, Zhao Liu*, Zhenping Feng, Experimental and Numerical Investigations into the Blade Tip Phantom Cooling Performance. ASME Journal of Engineering for Gas Turbines and Power,2022, 144, p. 071013. DOI: 10.1115/1.4054525.1.732, Q3
  9. Weixin Zhang, Feng Li, Zhe Jia, Zhao Liu*, Zhenping Feng, Yi Zhang, Experimental study on performance verification test of optimized film cooling holes in a linear cascade. Applied Thermal engineering, 2022, 212, p. 118574. DOI: 10.1016/j.applthermaleng.2022.118574. (WOS:000800034600002), 6.465, Q1

  1. Feng Li, Haifeng Wang, Zhao Liu*, Zhenping Feng, Yan Shi, Comparisons of Blade Tip Phantom Cooling Effectiveness for Two Tip Structures with Three Tip Clearances. Applied Thermal engineering, 2022, 202, p. 117868. DOI: 10.1016/j.applthermaleng.2021.117868. (WOS: 000742703200002), 6.465, Q1
  2. Feng Li, Zhe Jia, Weixin Zhang, Zhao Liu*, Zhenping Feng, Experimental Comparisons of Film Cooling Performance for the Multi-Cavity Tips at Two Different Tip Gaps. International Journal of Heat and Mass Transfer, 2022, 187, p. 122566. DOI： 10.1016/j.ijheatmasstransfer.2022.122566 (WOS: 000755665000008), 5.431, Q1

 

2021年：

  1. F. Li, Z. Liu, Z. Feng, Film cooling and aerodynamic performance on multi-cavity squealer tip of a turbine blade, Proceeding of American Society of Mechanical Engineers Turbo Expo2021, 2021, GT2021-59993.
  2. F. Li, Z. Liu, Z. Feng, Impact of blade leading edge film coolant on the blade tip phantom cooling, IOP Conference Series: Materials Science and Engineering, 2021, 1081, p.012048.
  3. 张韦馨, 刘战胜, 杨星, 刘钊, 丰镇平．射流角和质量流量比对涡轮端壁气膜冷却特性的影响．西安交通大学学报. 2021, 55(4). 网络首发论文
  4. Li Feng, Liu Zhao, Feng Zhenping. Turbine Blade Tip and Casing Phantom Cooling from Blade Surface Film Coolant. AIAA Journal of Thermophysics and Heat Transfer. 2021, 35(2):210-224. SN8LE (WOS:000658537100002)
  5. 张志欣, 李冯, 刘钊, 丰镇平. 气膜孔角度对动叶前缘冲击／气膜复合冷却的影响. 工程热物理学报, 2021, 42(1):130-135.
  6. 刘钊, 贾哲, 张志欣, 丰镇平. 透平动叶前缘冲击－气膜复合冷却与旋流－ 气膜复合冷却的热流耦合对比研究. 西安交通大学学报, 2021, 55(4):116-125.

 

2020年：

  1. Liu Zhao, Li Feng, Zhang Zhixin, Feng Zhenping*, Simon Terrence. Conjugate Heat Transfer Predictions on Combined Impingement and Film Cooling of a Blade Leading Edge Model [J]. Heat Transfer Engineering, 2020, July. (SCI: MN6PB，国际知名期刊)
  2. Yang Xing, Liu Zhansheng, Zhao Qiang, Liu Zhao, Feng Zhenping,* Simon Terrence. Comparisons of Endwall Overall Effectiveness from Two Film Hole Distribution Patterns at Low and High Exit Mach Numbers. ASME Journal of Turbomachinery, 2020, 142, 101007. (SCI: 已录用，最具影响力期刊)
  3. Wu Bin, Yang Xing, Liu Zhao, Feng Zhenping, Effect of Ribs on Heat Transfer and Pressure Drop in a U-Bend Channel with Double-Layer, Dome-Shaped Turning Vane. ASME Turbo Expo, Paper No. GT2020-15980.
  4. Liu Zhansheng, Yang Kefeng, Yang Xing, Liu Zhao, Feng Zhenping, Optimization of Film Cooling Holes for Enhancing Cooling Effectiveness Under Variable Coolant Inlet Pressure Ratios. ASME Turbo Expo, Paper No. GT2020-14989.
  5. 刘钊, 张韦馨, 刘战胜, 杨星, 丰镇平. 一种端壁气膜孔布置结构. 申请号: 202010611065.5. 授权号：CN111779548B, 专利号：ZL202010611065.5.
  6. Li Feng, Liu Zhao, Feng Zhenping. Impact of Blade Leading Edge Film Coolant on the Blade Tip Phantom Cooling, Proceedings of the Fourth Chinese International Turbomachinery Conference, CITC 202009917.
  7. 张韦馨, 张祎, 刘钊, 丰镇平. 基于RBF 神经网络的平板气膜冷却全局优化研究. 工程热物理学会年会热机气动热力学分会. 2020.

2019年：

 

[1]      Liu Zhao; Zhang Zhixin; Li Feng; Feng Zhenping*; Terrence W. Simon. Conjugate Heat Transfer Predictions on Impingement and Film Composite Cooling of Blade Leading Edge Model. 5th International Workshop on Heat/Mass Transfer Advances , Novosibirsk, Russia, 2019-8-13至2019-8-16.  其他 .

[2]      Yang, Xing; Liu, Zhansheng; Zhao, Qiang; Liu, Zhao; Feng, Zhenping*; Guo, Fushui; Ding, Liang; Simon, Terrence. Conjugate heat transfer measurements and predictions for the vane endwall of a high-pressure turbine with upstream purge flow. International Journal of Heat and Mass Transfer, 2019, 140: 634-647.

[3]      Yang, Xing; Liu, Zhao; Liu, Zhansheng; Feng, Zhenping*; Simon, Terrence. Turbine platform phantom cooling from airfoil film coolant, with purge flow. International Journal of Heat and Mass Transfer, 2019, 140: 25-40.

[4]      Zhao Qiang; Yang Xing; Liu Zhao; Feng Zhenping*; Terrence W. Simon. Controlling Leakage Flows Over a Rotor Blade Tip Using Air-Curtain Injection：Part II —— Rotor Casing Film Cooling. ASME Turbo EXPO, Phoenix，Arizona，USA, 2019-6-17至2019-6-21.  EI.

[5]      Yang, Xing; Liu, Zhansheng; Zhao, Qiang; Liu, Zhao; Feng, Zhenping*; Guo, Fushui; Ding, Liang; Simon, Terrence. Experimental and numerical investigations of overall cooling effectiveness on a vane endwall with jet impingement and film cooling. Applied Thermal Engineering, 2019, 148: 1148-1163.  SCIE.

[6]      Yang, Xing; Liu, Zhao; Liu, Zhansheng; Simon, Terrence; Feng, Zhenping*. 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, 11(1): 0-011008.  SCIE.

[7]      Yang, Xing; Liu, Zhansheng; Zhao, Qiang; Liu, Zhao; Feng, Zhenping*; Guo, Fushui; Ding, Liang. Measurements of detailed heat transfer characteristics on a high-pressure turbine vane endwall with coolant injection. Experimental Thermal and Fluid Science, 2019, 109: 0-UNSP 109888.  SCIE.

[8]      肖坤; 何娟; 刘钊; 丰镇平*. 交叉扭转椭圆气膜孔冷却机理研究. 2019年中国工程热物理学会热机气动热力学和流体机械学术会议, 北京, 2019-10-18至2019-10-20

[9]      张志欣; 李冯; 刘钊*; 丰镇平. 气膜孔角度对透平动叶前缘冲击/气膜复合冷却的影响. 2019 年中国工程热物理学会热机气动热力学和流体机械学术会议, 北京, 2019-10-18至2019-10-20.

[10]   张韦馨; 刘战胜; 杨星; 刘钊*; 丰镇平. 涡轮端壁离散气膜孔气膜冷却特性的数值研究. 2019 年中国工程热物理学会热机气动热力学和流体机械学术会议, 北京, 2019-10-18至2019-10-20.

[11]   Yang, Xing; Zhao, Qiang; Liu, Zhao; Feng, Zhenping*; Simon, Terrence W. Controlling Leakage Flows over a Rotor Blade Tip Using Air-Curtain Injection: Part I - Aero-Thermal Performance of Rotor Tips. ASME Turbo Expo: Turbomachinery Technical Conference and Exposition, 2019-6-17至2019-6-21.  ISTP.

 

 

2018年：

[1]      Zhansheng Liu; Xing Yang; Chun Gao; Zhao Liu; Zhenping Feng*. Aero-Thermal Coupled Design Optimization of the Non-Axisymmetric Endwall for a Gas Turbine Blade. ASME Turbo EXPO, Oslo, Norway, 2018-6-11至2018-6-15.  EI.

[2]      Bin Wu; Xing Yang; Lv Ye; Zhao Liu; Yu Jiang; Qiang Zhao; Zhenping Feng*. Flow and Heat Transfer Characteristics in Models of Turbine Blade Tip-Walls With Three Kinds of Turning Vanes. ASME Turbo EXPO, Oslo, Norway, 2018-6-11至2018-6-15.  EI.

[3]      Yang Xing; Liu Zhao; Liu Zhansheng; Feng Zhenping*; Simon Terrence. Combustor Wall Coolant Discharge Effects on Turbine Vane Endwall Curtain Cooling. AIAA Journal of Thermophysics and Heat Transfer, 2018, 2018(1): 1-13.  SSCI.

[4] 杨星; 刘战胜; 赵强; 刘钊; 丰镇平*. 叶栅进口雷诺数对涡轮端壁耦合换热影响的实验研究.中国工程热物理学会年会, 西安, 2018-10-26至2018-10-28 

 

2017年：

[1]      Yang Xing; Liu Zhao*; Liu Zhansheng; Feng Zhenping. Influence of Discharge from Combustor Walls on Curtain Cooling for a First-Stage Turbine Vane Endwall. 53rd AIAA/SAE/ASEE Joint Propulsion Conference, AIAA Propulsion and Energy Forum 2017, 2017-7-10至2017-7-12.  EI.

[2]      Ye, Lv; Liu, Zhao; Gao, Chun; Yang, Xing; Feng, Zhenping*. Numerical Study on Heat Transfer Performance of a New-proposed Pin-fin in an Internal Channel. ASME Turbo Expo: Turbine Technical Conference and Exposition, Charlotte, NC, 2017-6-26至2017-6-30.  EI.

[3]      Liu Zhao*; Li Jun; Feng Zhenping; Simon Terrence. A Numerical Study on the Effects of Number of Jets on Swirl Cooling of a Gas Turbine Blade Leading Edge. 2nd Thermal and Fluids Engineering Conference (TFEC) "Engineering Challenges for the Betterment of Society" and 4th International Workshop on Heat Transfer (IWHT) "Advances for Energy Conservation and Pollution Control", Las Vegas, 2017-4-2至2017-4-5.

[4]      Yang Xing; Liu Zhao; Liu Zhansheng; Feng Zhenping*. Interaction of Combustor Wall and Film Cooling onEndwall for a First-Stage Vane. 2nd Thermal and Fluids Engineering Conference (TFEC) "Engineering Challenges for the Betterment of Society" and 4th International Workshop on Heat Transfer (IWHT) "Advances for Energy Conservation and Pollution Control", Las Vegas, 2017-4-2至2017-4-5

[5]      杨星; 刘钊; 刘战胜; 丰镇平. 端壁错位对端壁泄漏流冷却的影响研究. 工程热物理学报, 2017, (04): 719-725.

[6]      武斌; 杨星; 赵强; 刘钊; 丰镇平. U型通道顶部流动换热的数值研究. 中国工程热物理学会热机气动热力学分会年会, 2017-11-10至2017-11-12.

[7]      刘战胜; 高春; 杨星; 刘钊; 丰镇平*. 代理模型在气膜孔优化中的应用研究. 中国工程热物理学会热机气动热力学分会年会, 2017-11-10至2017-11-12.

[8]      Yang Xing; Liu Zhansheng; Zhao Qiang; Liu Zhao; Feng Zhenping*. Experimental Investigation and Numerical Analysis on Heat Transfer of a Nozzle Guide Vane Endwall at Engine Representative Reynolds and Mach Numbers. Proceedings of Global Power and Propulsion Society, 2017-10-30至2017-11-1.

[9]    杨星; 刘钊; 刘战胜; 丰镇平. 端壁通道间隙对端壁泄漏流冷却的影响. 工程热物理学报, 2017, (01): 44-48.  EI,

 

2016年：

[1]      Saxena, Reema*; Alqefl, Mahmood H.; Liu, Zhao; Moon, Hee-Koo; Zhang, Luzeng; Simon, Terrence.  Contoured endwall flow and heat transfer experiments with combustor coolant and gap leakage flows for a turbine nozzle guide vane. ASME Turbo EXPO, Seoul, 2016-6-13至2016-6-17.  EI.

[2]      Liu, Zhao; Yang, Xing; Li, Jun; Feng, Zhenping*; Simon, Terrence. Effect of Bleed Position and Bleed Angle on Impingement Cooling of a Spherical-Dimpled Surface. ASME Turbo EXPO, Seoul, SOUTH KOREA, 2016-6-13至2016-6-17.  EI.

[3]      Yang, Xing; Liu, Zhao; Liu, Zhansheng; Wu, Bin; Feng, Zhenping*. Influence of Jet Impingement Configurations and Aerothermal Variables on Film Cooling. ASME Turbo EXPO, Seoul, 2016-6-13至2016-6-17.  EI.

[4]      Ye, Lv; Liu, Zhao; Wang, Xiangyu; Feng, Zhenping*. Numerical Study on Flow and Heat Transfer of a Cooled First Stage Vane of a Gas Turbine. ASME Turbo EXPO, Seoul, 2016-6-13至2016-6-17.  EI.

[5]      杨星; 刘钊; 刘战胜; 丰镇平. 端壁错位对端壁泄漏流冷却的影响研究. 2016年中国工程热物理学会热机气动热力学分会年会, 无锡, 2016-11-22至2016-11-25

[6]      叶绿; 汪翔宇; 刘钊; 丰镇平. 燃机透平第一级静叶复合冷却数值研究. 2016年中国工程热物理学会热机气动热力学年会, 无锡, 2016-11-22至2016-11-25.

 

[7]      Liu, Zhao*; Li, Jun; Feng, Zhenping; Simon, Terrence. Numerical study on the effect of jet spacing on the Swirl flow and heat transfer in the turbine airfoil leading edge region. Numerical Heat Transfer Part A-Applications, 2016, 70(9): 980-994.  SCIE.

 

2015年：

[1]      Yang, Xing; Liu, Zhao*; Feng, Zhenping. Numerical Evaluation of Novel Shaped Holes for Enhancing Film Cooling Performance. Journal of Heat Transfer-Transactions of the ASME, 2015, 137(7).  SCIE.

[2]      Yang, Xing; Liu, Zhao; Feng, Zhenping*. Effect of Film Extraction on Impingement Heat Transfer Characteristics of Jet Arrays on Spherical-Dimpled Surfaces. ASME TURBO EXPO, Montreal, 2015-6-15至2015-6-19.  EI.

[3]      刘战胜; 杨星; 邵帅; 刘钊; 丰镇平. 基于神经网络的平板气膜孔冷却性能分析及优化研究.高等教育学会工程热物理专业委员会全国学术会议, 中国江苏扬州, 2015-5-9至2015-5-10

[4]      刘钊*; 李军; 丰镇平. 叶片前缘旋流冷却的数值研究. 2015年中国工程热物理学会热机气动热力学分会, 2015-11-27至2015-11-29

[5]      Yang, Xing; Liu, Zhao*; Liu, Zhansheng; Feng, Zhenping. Numerical analysis on effects of coolant swirling motion on film cooling performance. International Journal of Heat and Mass Transfer, 2015, 90: 1082-1089.  SCIE.

[6]      Liu, Zhao; Li, Jun; Feng, Zhenping*; Simon, Terrence. Numerical study on the effect of jet nozzle aspect ratio and jet angle on swirl cooling in a model of a turbine blade leading edge cooling passage. International Journal of Heat and Mass Transfer, 2015, 90: 986-1000.  SCIE.

[7]      Yang Xing; Liu Zhao; Liu Zhansheng; Feng Zhenping*. Computational study on effects of purge flow on endwall film cooling and blade suction side phantom cooling. Proceedings of IWHT2015，3nd International Workshop on Heat Transfer Advances for Energy Conservation, 2015-10-16至2015-10-19

[8]      王昌叶; 刘钊*; 叶绿; 丰镇平. 叶片冲击/气膜复合冷却的数值研究. 工程热物理学报, 2015, (01): 55-59.

[9]      Liu, Zhao; Li, Jun; Feng, Zhenping*. Numerical Study of Swirl Cooling in a Turbine Blade Leading-Edge Model. Journal of Thermophysics and Heat Transfer, 2015, 29(1): 166-178. SCIE.

[10]   Yang Xing; Liu Zhao; Feng Zhenping. Effect of Film Extraction on Impingement Heat Transfer Characteristics of Jet Arrays on Spherical-Dimpled Surfaces. ASME Turbo EXPO, Montréal, Canada, 2015-6-15至2015-6-19.

[11]   Liu Zhao, Ye Lv, Yang Xing, Feng Zhenping *. Effect of Attack Angle and Jet Height on  Impingment and Film Composite Cooling of Turbine Blade Leading Edge, 2015, ISABE-20109.

 

2014年：

[1]      刘娜; 刘钊; 丰镇. U型通道内部流动与换热的数值研究. 工程热物理学报, 2014, (09): 1733-1738.  其他 .

[2]      Liu, Zhaofang; Liu, Zhao; Feng, Zhenping*. Unsteady Analysis on the Effects of Tip Clearance Height on Hot Streak Migration Across Rotor Blade Tip Clearance. Journal of Engineering for Gas Turbines and Power-Transactions of the ASME, 2014, 136(8).  SCIE.

[3]      Liu, Zhao*; Ye, Lv; Feng, Zhenping. Numerical Study of Impingement and Film Composite Cooling on Blade Leading Edge. ASME Turbo EXPO, Dusseldorf, 2014-6-16至2014-6-20.

[4]      杨星; 刘钊; 丰镇平. 燃气轮机透平叶片传热和冷却研究:端壁冷却. 热力透平, 2014, (02): 0-85.  其他 .

[5]      刘钊; 杨星; 丰镇平. 燃气轮机透平叶片传热和冷却研究:气膜冷却. 热力透平, 2014, (01): 1-9.  其他 .

[6]      Liu, Zhao; Ye, Lv; Wang, Changyee; Feng, Zhenping*. Numerical simulation on impingement and film composite cooling of blade leading edge model for gas turbine. Applied Thermal Engineering, 2014, 73(2): 1432-1443.  SCIE.

 

[7]      杨星; 刘钊; 叶绿; 刘战胜; 丰镇平. 内流环境对气膜冷却性能的影响. 2014中国工程热物理学术年会, 西安, 2014-10-30至2014-11-2

 

2013年：

[1]      刘娜; 刘钊*; 丰镇平. 燃气透平叶片内部U型通道流动与顶部换热的数值研究. 2013年中国工程热物理学会热机气动热力学分会, 2013-9-25至2013-9-27.

[2]      王昌叶; 刘钊*; 叶绿; 丰镇平. 实际燃气轮机透平叶片冲击/气膜复合冷却的数值研究. 2013年中国工程热物理学会热机气动热力学分会, 呼和浩特, 2013-9-25至2013-9-27.

[3]      王昌叶; 刘钊*; 叶绿; 丰镇平. 叶片前缘模型冲击气膜复合冷却的数值研究. 2013年中国工程热物理学会热机气动热力学分会, 呼和浩特, 2013-9-25至2013-9-27.

[4]      Liu Zhao*; Li Jun; Feng Zhenping. Numerical Study on the Effect of Jet Slot Height on Flow and Heat Transfer of Swirl Cooling in Leading Edge Model for Gas Turbine Blade. ASME Turbo Expo 2013, 2013-6-3至2013-6-7.  EI.

[5]      Liu, Zhaofang*; Liu, Zhao; Feng, Zhenping. Unsteady analysis on the effects of tip clearance height on hot streak migration across rotor blade tip clearance. ASME TURBO EXPO, San Antonio, TX, 2013-6-3至2013-6-7.  EI.

[6]      刘钊; 杨星; 丰镇平. 燃气轮机透平叶片传热和冷却研究:内部冷却. 热力透平, 2013, (04): 265-275.  

 

2011年前：

[1]      Liu, Zhao; Feng, Zhenping*; Song, Liming. Numerical study on flow and heat transfer characteristics of swirl cooling on leading edge model of gas turbine blade. ASME TURBO EXPO, Vancouver, 2011-6-6至2011-6-10.  EI.

[2]      赵晶金; 刘钊; 丰镇平; 余小兵. 新型反对称涡气膜冷却结构设计及其数值研究. 工程热物理学报, 2011, (05): 763-766.  其他 .

[3]      Liu, Zhao; Feng, Zhenping*. Numerical simulation on the effect of jet nozzle position on impingement cooling of gas turbine blade leading edge. International Journal of Heat and Mass Transfer, 2011, 54(23-24): 4949-4959. SCIE.

[4]      Liu, Zhao*; Feng, Zhenping; Song, Liming. Numerical Study of Flow and Heat Transfer of Impingement Cooling on Model of Turbine blade Leading Edge. ASME TURBO EXPO, Glasgow, SCOTLAND, 2010-6-14至2010-6-18.  EI.

[5]      刘钊; 丰镇平; 宋立明. 实际叶片前缘冲击冷却流动和换热的数值研究. 西安交通大学学报, 2010, (01): 5-9+20

[6]      陈昌山, 刘钊, 丰镇平. 肋片角度和旋转工况对叶片内部U型通道流动与换热影响的研究. 2010年中国工程热物理学会热机气动热力学分会会议论文.

[7]      刘钊, 宋立明, 丰镇平. 射流孔直径对透平叶片前缘内部流动和换热的影响. 2009年中国工程热物理学会热机气动热力学分会会议论文.

 

[8]      李海朋, 刘钊, 丰镇平. 两种波纹板通道内的流动及换热比较.工程热物理学报, 2008, 29(10):1755-1758.