[1] Yuefeng Huang, Zihan Zhang, Kun He, Xin Yan*. Enhanced Film Cooling Effect Downstream a Cylindrical Hole Using SDBD and DBD-VGs Plasma Actuations, ASME Paper GT2021-59413
[2] Sadam Hussain, Xin Yan*. Effect of Vortex Generators and Ramp on Endwall Film Cooling Near Blade Leading Edge, ASME Paper GT2021-59530
[3] Xin Yan. Very Large Eddy Simulation of Film Cooling Effectiveness on Trailing Edge Cutback, ASME Paper GT2020-15780. (EI: 20210509838065)
[2] Ruiqin Wang, Xin Yan*. Background-Grid Based Mapping Approach to Film Cooling Meshing-Part I: Strategies and Test Cases, ASME Paper GT2020-15768. (EI: 20210509841991)
[3] Ruiqin Wang, Xin Yan*. Background-Grid Based Mapping Approach to Film Cooling Meshing-Part II: Applications in Vane with Landed Trailing-Edge Cutback, ASME Paper GT2020-15093. (EI: 20210509842050)
[4] Ruiqin Wang, Xin Yan*. Background-Grid Based Mapping Approach to Film Cooling Meshing-Part III: Applications in a Full-Cooled Turbine Vane, ASME Paper GT2020-15092. (EI: 20210509842049)
[5] Mingliang Ye, Xin Yan*. Investigations of Heat Transfer and Film Cooling Effect on a Worn Squealer Tip, ASME Paper GT2020-14835. (EI: 20210509842040)
[6] Sadam Hussain, Xin Yan*. Implementation of Hole-Pair in Ramp to Improve Film Cooling Effectiveness on Plain Surface, ASME Paper GT2020-14838. (EI: 20210509842042)
[7] Xin Yan*, Yabo Wang, Kang Zhang, Xinbo Dai, Kun He. Investigations Into Aerodynamic Performance of Turbine Stages with Flexible Shroud Seals, ASME Paper GT2020-14329, 2020. (EI: 20210509838665)
[8] Xin Yan, Xinbo Dai. Effects of Labyrinth fin wear on Aerodynamic Performance of Turbine Stages-Part I: Bending Damages, ASME Paper GT2019-90152, 2019. (EI: 20194907782526 )
[9] Xinbo Dai, Xin Yan. Effects of Labyrinth fin wear on Aerodynamic Performance of Turbine Stages-Part II: Mushrooming Damages, ASME Paper GT2019-90153, 2019. (EI: 20194907782527)
[11] Xin Yan, Xinbo Dai, Kang Zhang, Jun Li, Kun He. Influence of hole-pattern stator on leakage performance of labyrinth seals, ASME Paper GT2018-75349, 2018. (EI:20184005897523)
[12] Jun Li, Yuanqiao Zhang, Xin Yan and Zhigang Li. Investigations on the Leakage Flow Characteristics of the Brush Seal with Annular Pressure Reduction Groove, 23rd International Conference of the International Society of Air Breathing Engines(ISABE), ISABE-2017-21331
[13] Kang Zhang, Xinbo Dai, Xin Yan*, Jun Li. Effect of Stator Rub Grooves on Leakage Performance of a Stepped Labyrinth Seal [C], 2017, Proceedings of Shanghai 2017 Global Power and Propulsion Forum, GPPS-2017-130. （通讯作者）
[14] Xin Yan, Xiuxiu Chen, Kun He. Influence of shroud Seal Dimensions on Aerodynamic Performance of Steam Turbine Stages: Part I-Honeycomb Seal [C], ASME Paper GT2016-56917, 2016. （EI：20164202925418）
[15] Xin Yan, Xiuxiu Chen, Kun He. Influence of shroud Seal Dimensions on Aerodynamic Performance of Steam Turbine Stages: Part II- Hole-pattern Seal [C], ASME Paper GT2016-56921, 2016. （EI：20164202925419）
[16] Xin Yan, Yizhi Fan, Xianyou Shang, Kun He, Jun Li, Zhenping Feng. Theoretical investigations on water condensation in main steam pipe [C], ASME Paper GT2012-69567, 2012. (EI源刊：20133316600296)
[17] Xin Yan, Lijie Lei, Jun Li, Zhenping Feng. Effect of bending and mushrooming damages on heat transfer characteristic in labyrinth seals, ASME Paper TBTS2013-2012.
[18] Zhigang Li, Jun Li, Xin Yan, Zhenping Feng, Hiroharu Ohyama, Ming Zhang. Investigations on the Flow Pattern and Aerodynamic Performance of Last Stage and Exhaust Hood for Large Power Steam Turbines, Proceedings of the ASME Turbo Expo 2012-Power for Land, Sea, and Air, Copenhagen, Denmark, GT2012-69291.
[19] Wenhao Huo, Jun Li, Xin Yan, Zhenping Feng. Numerical Investigations on the Steam Cooling Performance of the First Two Middle Pressure Turbine Stages for Ultra-Supercritical Steam Turbines, Proceedings of the ASME Turbo Expo 2012-Power for Land, Sea, and Air, Copenhagen, Denmark, GT2012-69302.
[20] Jun Li, Xin Yan, Liming Song, Jinshan Wang, Zhenping Feng. Effects of squealer rim thickness on the leakage flow and heat transfer characteristics of the gas turbine blade tip[C], AJCPP2012-009, 2012.
[21] Jia Liu, Jun Li, Xin Yan, Zhenping Feng. Effect of Rotor Blade Tip Cavity Flow on Aerodynamic Performance of Turbine Stages [C]. AJCPP2012-049, 2012.
[22] Jun Li, Xin Yan, Liming Song, Shengru Kong, Zhenping Feng. Numerical Investigations on the Leakage Flow Characteristics of Different Honeycomb Seal Configurations[C], International Gas Turbine Congress, IGTC2011-0114,
[23] Jun Li, Xin Yan, Liming Song, Shaojun Li, Zhenping Feng. Effects of Rotor Tip Leakage on the Unsteady Flow Fields of Stator Blade in a One and Half Turbine Stage [C], International Gas Turbine Congress, IGTC2011-0117, Osaka, Japan, 2011.
[24] Jun Li, Zhigang Li, Xin Yan, Liming Song, Zhenping Feng. Effect of cell diameter and depth on the leakage flow characteristics of honeycomb seals[C], ICFD Conference,
[25] Jun Li, Yong Jiang, Xin Yan, Liming Song, Zhenping Feng. Numerical investigations on the aerodynamic performance of throttle governing stage for large power steam turbines[C]. ICFD
[26] Xin Yan, Jun Li, Zhenping Feng. Numerical investigations on the leakage flow and heat transfer characteristics of a stepped labyrinth seal[C]. The 7th International Symposium on Heat Transfer,
[27] Xin Yan, Jun Li, Yonghui Xie, Zhenping Feng, Gangyun Zhong, Qilin Wu, Jianlu Wang. Computational fluid dynamics analysis approach to the aerodynamic performance of a nozzle controlling stage for a 600MW steam turbine [C & M]. Proceedings of the International Conference on Power Engineering 2007,
[28] Jun Li, Xin Yan, Guojun Li, Zhenping Feng. Effect of pressure ratio and sealing clearance flow characteristics in the rotating honeycomb labyrinth seal[C]. ASME Paper GT2007-27740, 2007. (EI：073910824299).
[29] Jun Li, Xin Yan, Zhenping Feng. Numerical investigations on the flow characteristics in the labyrinth seals with the smooth and honeycomb lands [C]. AJCPP2006-22114, 2006.
[30] Li Jun, Yan Xin, Feng Zhenping. Effects of Pressure Ratio and Fin Pitch on Leakage Flow Characteristics in High Rotating Labyrinth Seals[C]. ASME Paper GT2006-91145, 2006. (EI:064610237402).
[31] Jun Li, Xin Yan, Qiang Lv, Yonghui Xie, Zhenping Feng. The effect of the shrouded rotor blade tip leakage flow on the aerodynamic performance of a one and half turbine stage [C & M]. Proceedings of the International Conference on Power Engineering 2007,
[32] Huo W, Li J, Yan X, et al. Numerical Investigations on the Steam Cooling Performance of the First Two Middle Pressure Turbine Stages for Ultra-Supercritical Steam Turbines, 2012. ASME Paper GT2012-69302.
[33] Xin Yan, Kun He, Jun Li. Effect of Rub Mushrooming Damage on the Leakage Flow Characteristics of Labyrinth Seal[C], Eleventh International Conference on Flow Dynamics, Oct. 8-10, 2014,
[34] Zhang YQ, Li J, Yan X, Li ZG. Experimental and numerical investigations on leakage flow characteristics of two kinds of brush seals[C]. ASME Paper GT2018-76235, 2018. (EI：20184005897536)
[35] MA DQ, Zhang YQ, Li ZG, Li J, Yan X. Numerical Investigations on the Leakage Flow Characteristics of Brush Seal Based on the 3d Staggered Tube Bundle Model[C]. ASME Paper GT2020-14590, 2020. (EI会议文章)
[36] Zhang YQ, Li J, Li ZG, Song LM, Yan X. Effect of upstream deflector plate on the leakage flow and heat transfer characteristics of brush seal with annular groove in backing plate[C]. 24th International Society for Air Breathing Engines Conference, ISABE-2019-24096,
[37] Zhang YQ, Ma DQ, Li J, He Y, Ji JJ, Sun B, Li ZG, Yan X. Effect of the fence height on the leakage flow characteristics of brush seals[C]. Global Power & Propulsion Society:
[38] Li J, Ma DQ, Zhang YQ, He Y, Ji JJ, Sun B Li ZG, Yan X. Experimental and numerical investigations on the leakage flow characteristics of zero and clearance brush seals[C]. 12th International Gas Turbine Congress, IGTC-2019-0027,