个人简历

陈绍文，男，汉族。哈尔滨工业大学能源科学与工程学院，副院长。
cswemail@hit.edu.cn
先后主持承担“两机”重大专项课题、子课题，xx国家重大专项xx发动机子课题，国家自然科学青年（一项）和面上基金（两项），中国博士后科学基金，黑龙江省博士后科研启动基金，哈尔滨工业大学科研创新基金，参与过包括国家科技部973项目、国家科技部863项目、国家自然科学基金重点项目和国防基础科研项目等国家级项目的相关科研工作。同时承担相关横向课题若干。
教育经历
1998年-2002年, 就读于哈尔滨工业大学, 本科
2002年-2007年, 就读于哈尔滨工业大学, 硕博连读, 硕士&博士
工作经历
2007年7月-2018年12月 哈尔滨工业大学能源科学与工程学院，讲师、副教授、教授
2014年4月-至今 哈尔滨工业大学能源科学与工程学院，博士生指导教师
2015年1月-2016年1月 美国弗吉尼亚联邦州立大学工程学院机械与核工程系，访问学者
2016年7月-2017年7月 哈尔滨工业大学人事处处长助理（挂职）
2018年10月-2018年11月 美国明尼苏达大学访问交流
2019年10月-2020年7月 工业和信息化部产业发展促进中心
2020年6月-至今 哈尔滨工业大学能源科学与工程学院，副院长
荣誉称号
2011年 获哈尔滨工业大学青年教师教学基本功竞赛二等奖
2012年 获黑龙江省科技创新创业共享服务先进个人
2015年 被评为《推进技术》优秀审稿人
2018年 被评为哈尔滨工业大学招生宣传优秀个人
2018年 被评为哈工大先进个人
2020年 被评为《工程热物理学报》突出贡献者
获得奖励
1. 黑龙江省自然科学一等奖 2016
2. 哈工大青年教师教学基本竞赛二等奖 2011
3. 国防科技进步二等奖 2008
4. 江苏苏州吴中区创新创业领军人才 2011
5. 姑苏创新创业领军人才 2011
课程及研究方向
讲授的课程：
本科专业课：《燃气轮机原理》《飞机电推进装置及结构》
本科夏季小学期课：《风洞理论与测试技术》
本科创新研修课：《先进航空发动机内部流动控制技术》
研究生一年级：《实验空气动力学》、《应用型硕士实践环节-低速叶栅内流动机理及二次流控制》
同时指导本科生科技创新大赛、大学生节能减排大赛等。
研究方向：
地面燃气轮机及航空发动机；叶轮机械（压气机/涡轮/风机）内气动性能分析与优化设计；压气机复杂三维流动主、被动控制技术；先进风洞实验与测试技术应用。
教学研究项目：
2016年度研究生教育改革研究项目-《基于翻转课堂模式的专业硕士研究生实践课程建设与改革》
2019年度校级教学自制设备研究项目-《*****》

研究领域

"先进风洞实验与测试技术理论与应用研究（压气机/涡轮平面/扇形叶栅，风机、气动模型等）
叶轮机械复杂三维流动主、被动控制技术研究（附面层抽吸、弯曲叶片、脉动射流/抽吸、非对称端壁、叶顶小翼凹槽）
燃气轮机内颗粒摄入与污垢沉积影响研究（压气机/风扇/涡轮/风机）
叶轮机械内气动性能分析与优化设计（压气机/风扇/涡轮/风机）
高超声速气动热力学研究及优化设计"

近期论文

Xia G., Li H., Ding Y., Wei L., Chen S., Yu D. Performance Optimization of a Krypton Hall Thruster with a Rotating Propellant Supply. Acta Astronautica. Volume 171, June 2020, Pages 290-299.
Xia G., Li H., Zhu X., Ning Z., Chen S., Yu D., Zhou C. Effects of Rotating Supply Mode on the Ionization Parameters of a Krypton Hall Thruster. Vacuum, Volume 181, November 2020, 109664.
Sun S., Wang S., Chen S. Design, Modification and Optimization of an Ultra-High-Load Transonic Low-Reaction Aspirated Compressor. Aerospace Science and Technology. Volume 105, October 2020, 105975.
Zhang, H., Chen, S*. A Comparative Experimental Analysis of Two Unsteady Flow Control Methods in a Highly Loaded Compressor Cascade. Exp Fluids, 61, 132 (2020).
Jiang S., Yu J., Wang H., Chen F., Chen S., Song Y. Experimental Investigation of the Bending Clearance on the Aerodynamic Performance in Turbine Blade Tip Region. Energy, Volume 197, 15 April 2020, 117234.
Sun S., Wang S., Chen S. The Influence of Diversified Forward Sweep Heights on Operating Range and Performance of an Ultra-High-Load Low-Reaction Transonic Compressor Rotor.Energy,Volume 194, 1 March 2020, 116857.
Xia G., Ning Z., Zhu X.*, Wei L., Chen S*. and Yu D. Effect of Low-Frequency Oscillation on Plasma Focusing in Krypton Hall Thruster. Journal of Propulsion and Power, 2019, 36(6):1-8.
Xia G., Liu X., Li H., Ding Y., Wei L., Chen S., Yu D. Performance Improvement of Hall Thrusters with High Discharge Voltage.Vacuum,Volume 172, February 2020, 109052.
Jiang S., Ning Z., Xia G., Zhu X., Wei L., Chen S. and Yu D. Research on Beam-Focusing Characteristics of Krypton Hall Thruster. Plasma Phys. Rep. 45, 537–550 (2019).
Chen F., Yu J., Chen S., Song Y. Treatment and Optimization of Casing and Blade Tip for Aerodynamic Control of Tip Leakage Flow in a Turbine Cascade. Aerospace Science and Technology. Volume 86, March 2019, Pages 704-713.
Meng Q. H., Du X., Chen S. W.*, Wang S. T. Numerical Study of Dual Sweeping Jet Actuators for Corner Separation Control in Axial Compressor. Journal of Thermal Science. 2019. (Accepted)
Li W. H., Chen S. W.*, Liu H. Y., Zhou Z. H., Wang S. T. Effects of Double-Side Labyrinth Seals on Aerodynamic Performance in a Transonic Shrouded Turbine Stage. ASME Journal of Engineering for Gas Turbines and Power, 2020, 142(2): 021010-1-12.
Meng Q. H., Chen S. W.*, Ding S. L., Liu H. Y., Wang S. T. Large Eddy Simulation of Pulsed Blowing in a Supersonic Compressor Cascade. Journal of Applied Fluid Mechanics, 2019. (Accepted)
Chen S. W.*, Meng Q. H., Liu Y. Q., Liu H. Y., Wang S. T. Unsteady Numerical Simulation in a Supersonic Compressor Cascade with a Strong Shock Wave. International Journal of Turbo & Jet-Engines, 2019. (In Press, DOI: 10.1515/tjj-2019-0003)
Chen S. W.*, Li W. H., Meng Q. H., Zhou Z. H., Wang S. T. Effects of a Sweeping Jet Actuator on Aerodynamic Performance in a Linear Turbine Cascade with Tip Clearance, Proceedings of the Institution of Mechanical Engineers, Part G, Journal of Aerospace Engineering. 2019, 233(12): 4468-4481.
Sun S. J.*, Wang S. T., Chen S. W.*, Tao C., Cai L., Chen J. W. The Impact of Various Forward Sweep Angles on the Performance of an Ultra-High-Load Low-Reaction Transonic Compressor Rotor. Applied Thermal Engineering. 2019, 150 (2019): 953–966.
Zhou Z. H., Chen S. W.*, Li W. H., Wang S. T. Thermal Performance of Blade Tip and Casing Coolant Injection on a Turbine Blade with Cavity and Winglet-Cavity Tip. International Journal of Heat and Mass Transfer. 2019, 130(2019): 585-602.
Zhang H. X., Chen S. W.*, Wang S. T., Wang Z. Q. Numerical Study of Unsteady Pulsed Suction through Endwall Bleed Holes in a Highly Loaded Compressor Cascade. International Journal of Turbo & Jet-Engines, 2018. (In Press, DOI: 10.1515/tjj-2018-0035)
Zhang H. X., Chen S. W.*, Gong Y., Wang S. T., Wang Z. Q. Combined Application of Negative Bowed Blades and Unsteady Pulsed Holed Suction in a High-Load Compressor in Terms of Aerodynamic Performance and Energy Efficiency. Applied Thermal Engineering. 2018, 144 (2018): 291–304.
Chen S. W., Gong Y., Li W. H., Wang S. T., Wang Z. Q. Numerical Study of the Air Bleeding Caused Non-Uniformity in Axial Compressor. Journal of Thermal Science. 2020, 29(2020): 219-231.
Sun S. J.*, Chen S. W.*, Liu W., Gong Y., Wang S. T. Effect of Axisymmetric Endwall Contouring on the High-Load Low-Reaction Transonic Compressor Rotor with a Substantial Meridian Contraction. Aerospace Science and Technology. 2018, 81(2018): 78-87.
Chen S. W., Gong Y. Numerical Study of the Effects of Cartridge Shape on the Reverse Pulsed Flow Cleaning of Pleated Cartridge Filters, Proceedings of the Institution of Mechanical Engineers, Part E, Journal of Process Mechanical Engineering. 2019, 233(2): 371-383.
Zhang H. X., Chen S. W.*, Gong Y., Wang S. T. A Comparison of Different Unsteady Flow Control Techniques in a Highly Loaded Compressor Cascade, Proceedings of the Institution of Mechanical Engineers, Part G, Journal of Aerospace Engineering. 2019, 233(6): 2051-2065.
Chen S. W., Meng Q. H., Li W. H., Zhou Z. H., Wang S. T. Experimental Study on Axially Non-Uniform Clearances in a Linear Turbine Cascade with a Cavity Squealer Tip, Proceedings of the Institution of Mechanical Engineers, Part G, Journal of Aerospace Engineering. 2019, 233(5): 1465-1655.
Zhang H. X., Chen S. W.*, Meng Q. H., Wang S. T. Using Unsteady Pulsed Suction through Endwall Bleeding Holes in a Highly Loaded Compressor Cascade. Aerospace Science and Technology. 2018, 72(2018): 455-464.
Zhou Z. H., Chen S. W.*, Wang S. T. Unsteady Study of Winglet Cavity Tip on Leakage Flow in a High Pressure Turbine Stage of Low-Aspect Ratio. Proceedings of the Institution of Mechanical Engineers, Part C, Journal of Mechanical Engineering Science. 2018, 232(20): 3708-3721.
Zhou Z. H., Chen S. W.*, Li W. H., Wang S. T., Zhou X. Experiment Study of Aerodynamic Performance for the Suction-Side and Pressure-Side Winglet-Cavity Tips in a Turbine Blade Cascade. Experimental Thermal and Fluid Science. 2018, 90(2018): 220-230.
Zhang H. X., Chen S. W.*, Gong Y., Wang S. T. Flow Control Using Unsteady Pulsed Holed Suction with Different Excitation Models in a Highly Loaded Compressor Cascade. Proceedings of the Institution of Mechanical Engineers，Part A, Journal of Power and Energy. 2018, 232(6): 593-607.
Zhou Z. H., Chen S. W.*, Wang S. T. Aerodynamic Optimization of Winglet-Cavity Tip in an Axial High-Pressure Turbine Stage. International Journal of Turbo & Jet-Engines, 2017. (In Press, DOI: 10.1515/tjj-2017-0038)
Ding J., Chen S. W., Cai L., Wang S. T., Wang Z. Q., Shen J. Q. The Synergistic Effect between Compound Lean and Aspiration on Aerodynamic Performance in Compressor Cascades, Proceedings of the Institution of Mechanical Engineers, Part G, Journal of Aerospace Engineering. 2018, 232(16): 3034-3048.
Chen S. W., Zhou Z. H., Meng Q. H., Wang S. T., Zhou X. Experiment Study of the Winglet-Cavity Tip on the Aerodynamic Performance in a Turbine Cascade. Proceedings of the Institution of Mechanical Engineers，Part A, Journal of Power and Energy. 2017, 231(7): 676-685.
Chen S. W., Chen D. Cleaning of Filter Cartridges with Convergent Trapezoidal Pleat Shape Via Reverse Multi-pulsing Jet Flow. Aerosol and Air Quality Research, 2017, 17(11): 2645-2658.
Zhou Z. H., Chen S. W.*, Wang S. T. Numerical Aerodynamic Optimisation of a Winglet-Cavity Tip in a High-Pressure Axial Turbine Cascade. Proceedings of the Institution of Mechanical Engineers，Part G, Journal of Aerospace Engineering. 2018, 232(4): 649-663.
Chen S. W., Chen D. Annular-slit Nozzles for Reverse Flow Cleaning of Pleated Filter Cartridges. Separation and Purification Technology, 177(2017): 182-191.
Chen S. W., Zhou Z. H., Wang S. T., Wang Z. Q. Numerical Investigation of Boundary Layer Suction on Certain Highly Loaded Aspirated Compressor at Low Speeds. Proceedings of the Institution of Mechanical Engineers，Part G, Journal of Aerospace Engineering. 2018, 232(1): 30-41.
Chen S. W., Wang Q. and Chen D. Effect of Pleat Shape on Reverse Pulsed-jet Cleaning of Filter Cartridges. Powder Technology, 2017, 305: 1-11.
Chen S. W., Chen D. Numerical Study of Reverse Multi-Pulsing Jet Cleaning for Pleated Cartridge Filters. Aerosol and Air Quality Research, 2016, 16(8): 1991-2002.
Chen S. W., Lan Y. H., Zhou Z. H., Wang S. T. Investigation of Positively Curved Blade in Compressor Cascade Based on Transition Model. International Journal of Turbo & Jet-Engines, 2016, 33(2): 161-173.
Chen S. W., Xu H., Sun S. J., Zhang L. X., Wang S. T. Influence of Additional Leading-Edge Surface Roughness on Performances in Highly Loaded Compressor Cascade. International Journal of Turbo & Jet-Engines, 2015, 32(2): 155-163.
Chen S. W., Xu H., Wang S. T., Wang Z. Q. Experimental Research of Surface Roughness Effects on Highly-Loaded Compressor Cascade Aerodynamics. Journal of Thermal Science, 2014, 23(4): 1-8.
Chen S. W., Sun S. J., Lan Y. H., Wang S. T. The Effect of different Clearance Geometry Configurations on Aerodynamic Performance in a High-load Compressor Cascade. Proceedings of the Institution of Mechanical Engineers，Part G, Journal of Aerospace Engineering, 2014, 228(8): 1425-1433.
Chen S. W., Sun S. J., Xu H., Wang S. T. Experimental Study of the Impact of Hole-type Suction on the Flow Characteristics in a High-load Compressor Cascade with a Clearance. Experimental Thermal and Fluid Science, 2013, volume 51, pp. 220-226.
Chen S. W., Shi H., Zhang C., Wang S. T., Wang Z. Q.. Study on Numerical Simulation of Fouling in Compressor Rotor. International Journal of Turbo & Jet-Engines, 2012, 29(3), 179-188.
Guo S., Chen S. W., Lu H. W., Song Y. P., Chen F.. Enhancing Aerodynamic Performances of a High-Turning Compressor Cascade via Boundary Layer Suction. Science in China Series E, 2010, 53(10): 2748-2755.
Guo S., Chen S. W., Song Y. P., Song Y. F., Chen F.. Experimental Investigation into Effect of Boundary Layer Suction on The Performance of Highly-loaded Compressor Cascade. Chinese Journal of Aeronautics. 2010, 23: 179~186.
Chen S. W., Chen F.. Analysis of Aerodynamic Performance in an Annular Compressor Bowed Cascade with Large Camber Angles. International Journal of Fluid Machinery and Systems. 2009, 1(2): 13-20.
Chen S. W., Chen F., WANG K. L., GU J., Wang Z. Q.. Aerodynamic Performance of Bowed Compressor Cascades with Different Camber Angles. Front. Energy Power Eng. China. 2008, 2(3): 306-312.
国际会议：
Chen S. W., Zhang H. X., Meng Q. H., Wang S. T., Wang Z.Q. A Combination Application of Negative Bowed Blade and Endwall Unsteady Pulsed Holed Suction In A Highly Loaded Compressor Cascade. ASME IGTI Paper, No. GT2018-75912, 2018.
Zhou Z. H., Wang S. T., Chen S. W.* Numerical Study of Blade Tip Cooling at High Speed Condition with Tip and Pressure-Side Coolant Injections. ASME IGTI Paper, No. GT2018-75915, 2018.
Meng Q. H., Chen S. W.*, Li W. H., Wang S. T. Numerical Investigation of a Sweeping Jet Actuator for Active Flow Control in a Highly Loaded Compressor Cascade . ASME IGTI Paper, No. GT2018-76052, 2018.
Sun S. J., Wang S. T., Chen S. W. Aerodynamic Design and Analysis of a Two-Stage High-Load Low-reaction Transonic Aspirated Counter-Rotating Compressor. ASME IGTI Paper, No. GT2017-64144, 2017.
Ding J., Du X. Chen S. W., Zhou X., Wang S. T., Shen J. Q. Influence of Tailored Boundary Layer Suction on Aerodynamic Performance in Bowed Compressor Cascades. ASME IGTI Paper, No. GT2017-63217, 2017.
Chen S. W., Zhou Z. H., Cui T., Wang J. S., Wang S. T. Effects of Tip Injection on Tip Clearance Flow in a Low-pressure Turbine Stator Cascade. ASME IGTI Paper, No, GT2014-25185, 2014.
Chen S. W., Sun S. J., Xu H., Zhang L. X., Wang S. T. Influence of Local Surface Roughness of Rotor Blades on Performance of an Axial Compressor Stage. ASME IGTI Paper, No, GT2013-94816, 2013.
Zhang L. X., Chen S. W.*, Xu H., Ding, J., Wang S. T. Effect of Boundary Layer Suction on Aerodynamic Performance of High-Turning Compressor Cascade. ASME IGTI Paper, No, GT2013-94907, 2013.
Ding J., Chen S. W.*, Xu H., Sun S. J., Wang S. T. Control of Flow Separations in Compressor Cascade by Boundary Layer Suction Holes in Suction Surface. ASME IGTI Paper, No. GT2013-94723, 2013.
Chen S. W., Zhang C., Shi H., Wang S. T., Wang Z. Q. Study on the Impact of Fouling on Axial Compressor Stage. ASME IGTI Paper, No. GT2012-68041, 2012.
Shaowen CHEN, Shuang Guo, Yufei Song, Fu CHEN. Effects of Boundary Layer Suction on the Flow Behavior of Highly-loaded Compressor Cascades. 9th IASIF Paper. Korea.
国内期刊：
孟庆鹤，李伟航，陈绍文，等. 扫频式射流对涡轮叶栅间隙泄漏流动影响的数值研究. 推进技术，2019（已录用）.
孟庆鹤，陈绍文，等. 直孔射流对压气机叶栅流场影响的实验研究. 推进技术，2019（已录用）.
孟庆鹤，陈绍文，等. 扫频式射流对设计工况压气机叶栅流动分离影响的数值研究. 推进技术，2019（已录用）.
孟庆鹤, 陈绍文, 刘宏言, 王松涛. 轴向非均匀凹槽叶顶的实验与数值研究. 航空动力学报, 2019, 34(8), 1813-1821.
张洪鑫，陈绍文, 等. 变攻角下端壁非定常脉动抽吸对高负荷压气机叶栅分性能的影响. 推进技术，2018（已录用）.
张洪鑫，陈绍文, 等. 孔式非定常脉动抽吸控制高负荷压气机叶栅内流动分离的参数研究. 推进技术，2019, 40(3): 552-560.
孟庆鹤, 陈绍文, 等. 变工况下轴向非均匀凹槽叶顶的实验研究. 工程热物理学报，2018, 39(11): 2398-2403.
周治华, 陈绍文, 李伟航, 崔 涛, 王松涛. 叶顶凹槽间隙气膜冷却的传热数值研究. 推进技术. 2018, 39(3): 575-582.
丁骏, 陈绍文, 王松涛等. 亚声速扩压叶栅中弯叶片积叠规律的研究. 推进技术. 2017, 38(3): 570-580.
周治华, 陈绍文, 兰云鹤, 崔 涛, 王松涛. 叶顶不同位置喷气对涡轮间隙泄漏流动的影响. 推进技术. 2016,37(4): 879-885.
张晓辉, 陈绍文, 李燕飞. 基于弯曲叶片的燃气涡轮导叶数值研究. 推进技术. 2016,37(3): 443-448.
张龙新, 杜鑫, 陈绍文, 等. 基于主/被动联合控制技术设计的高负荷扩压叶栅内部流场结构研究. 推进技术. 2015,36(11): 1662-1668.
张龙新, 王松涛, 陈绍文, 王仲奇. 亚声速低反力度吸附式压气机的非定常数值研究. 中国电机工程学报, 2015, 35(15): 3879-3885.
崔涛, 陈绍文, 周治华, 等. 深凹槽式涡轮叶顶间隙泄漏直列叶栅实验研究. 工程热物理学报, 2015, 36(9): 1902-1906.
周治华, 陈绍文, 兰云鹤, 王松涛. 间隙对某涡轮级流场及气动性能影响的数值研究. 中国电机工程学报, 2015, 35(5): 1176-1182.
陈绍文, 孙士珺, 兰云鹤, 周治华, 王松涛. 来流附面层对吸附式压气机叶栅影响的数值研究. 机械工程学报, 2014, 50(24): 158-163.
孙士珺, 陈绍文, 王春雪等. 孔式抽吸对带间隙高负荷压气机性能的影响. 推进技术. 2014,35(9): 1202-1208.
陈绍文, 兰云鹤, 王春雪等. 基于转捩的吸附式压气机正弯叶片数值研究. 推进技术. 2014, 35(9): 1188-1193.
陈绍文，孙士珺，韩东，徐皓，王松涛. 间隙大小对高负荷压气机叶栅流动特性影响的实验研究. 工程热物理学报. 2014, 35(1), 34-37.
丁骏, 陈绍文, 徐皓等. 采用附面层抽吸孔改善高负荷扩压叶栅性能的研究. 工程热物理学报. 2013, 34(12), 2237-2242.
张龙新，陈绍文，郭昊雁，杜鑫，王松涛. 端壁采用孔式抽吸对扩压叶栅气动性能的影响. 推进技术. 2013, 34(9): 1204-1208.
孙士珺, 陈绍文, 韩东, 徐皓, 王松涛. 附面层吸除对带间隙的高负荷压气机叶栅流动特性影响的实验研究. 工程热物理学报. 2013, 34(9), 1645-1648.
张龙新, 陈绍文, 孙士珺, 王松涛, 王仲奇. 污垢沉积对某轴流压气机中间两级性能影响的数值研究. 中国电机工程学报, 2012, 32(35), 130-136.
陈绍文, 张辰, 石慧, 王松涛, 王仲奇. 轴流压气机内污垢沉积影响的数值研究. 推进技术, 2012, 33(3), 377-383.
石慧, 陈绍文, 张辰, 王松涛, 王仲奇. 基于动叶污垢沉积的数值模拟. 航空动力学报, 2012, 27(5), 1061-1067.
陈绍文, 王松涛, 王仲奇. 正冲角下高负荷吸附式压气机叶栅数值研究. 机械工程学报, 2011, 47(20), 177-182.
郭爽, 陈绍文, 陆华伟, 宋彦萍, 陈浮, 王仲奇. 组合抽吸对大转角扩压叶栅性能的影响. 航空动力学报. 2010, 25(12): 2697~2703.
陈绍文, 郭爽, 陈浮，王仲奇. 高负荷吸附式压气机叶栅开槽方案实验研究. 实验流体力学. 2010, 24(5): 26~30.
陈绍文, 郭爽, 陈浮，王仲奇. 局部附面层吸除对高负荷扩压叶栅气动性能的影响. 航空动力学报. 2010, 25(8): 1836~1841.
陈绍文, 郭爽, 宋宇飞, 陈浮. 局部附面层抽吸对高负荷扩压叶栅流动特性的影响. 工程热物理学报. 2010, 31(3): 407~410.
陈绍文, 郭爽, 宋宇飞, 陈浮, 刘顺隆. 附面层抽吸对高负荷压气机叶栅流场的影响. 推进技术. 2009, 30(5): 588~593.
陈绍文, 郭爽, 宋宇飞, 陈浮. 附面层抽吸对高负荷扩压叶栅三维流动及负荷的影响. 工程热物理学报. 2009, 30(9): 1479~1481.
郭爽, 陈绍文, 宋宇飞等. 附面层抽吸对高负荷扩压叶栅损失的影响. 工程热物理学报, 2009, 30(4): 574~576.
陈绍文, 郭爽, 陆华伟, 陈浮. 超高负荷吸附式压气机叶栅气动性能分析. 热能动力工程. 2009, 24(2): 167~171.
陈绍文, 卞兆喜, 刘顺隆. 冲角对高负荷正弯叶栅壁面静压影响的实验研究. 热能动力工程. 2008, 23(5): 468~472.
陈绍文, 陈浮, 王仲奇. 进口附面层对大转角弯曲扩压叶栅气动性能的影响. 航空动力学报. 2008, 23(7): 1225~1231.
陈绍文, 陈浮, 王仲奇. 变稠度大折转角弯曲扩压叶栅数值优化. 工程热物理学报. 2008, 29(2): 225~227.
陈浮, 陈绍文, 郭爽, 王仲奇. 高负荷弯曲扩压叶栅中旋涡流动的研究. 工程热物理学报. 2008, 29(1): 49~51.
陈绍文, 陈浮, 张晓辉, 王仲奇. 叶片弯曲对大转角压气机叶栅流场影响的研究. 推进技术. 2008, 29(3): 349~354.
陈浮, 陈绍文, 郭爽, 王仲奇. 高负荷压气机叶栅分离与流场结构研究. 工程热物理学报. 2007, 28 (S1): 117~120.
陈绍文, 陈浮, 冯冬民, 王仲奇. 叶片弯曲对不同折转角扩压叶栅冲角特性影响. 航空动力学报. 2007, 22(3): 406~410.
陈绍文, 陈浮, 王可立, 谷君, 王仲奇. 采用弯叶片的不同折转角压气机叶栅流场气动性能. 推进技术. 2007, 28(2): 170~175.
陈绍文, 佟勇. 近零冲角下达折转角正弯叶栅壁面静压的实验研究. 燃气涡轮试验与研究. 2006, 19(4): 1~5.
陈浮, 陈绍文, 王可立, 谷君, 王仲奇. 大折转角弯曲扩压叶栅变冲角性能研究. 工程热物理学报. 2006, 27(2): 220~222.
陈浮, 陈绍文, 赵桂杰, 王仲奇. 不同折转角弯曲扩压叶栅性能数值研究及优化设计. 热能动力工程. 2005, 20(3): 258~261.
陈绍文, 陈浮, 宋彦萍, 徐文远, 王仲奇. 某型低压涡轮导向器叶栅改型实验研究. 工程热物理学报. 2005, 26(S1): 73~76.
陈绍文, 陈浮, 徐文远, 王仲奇. 变攻角下低压涡轮导向器二次流的实验研究. 燃气涡轮试验与研究. 2005, 18(4): 15~19.
期刊审稿人：《推进技术》《工程热物理学报》《湖南大学学报》《大连海事大学学报》《国防科技大学学报》《Experimental Thermal and Fluid Science》《Aerosol Science & Technology》《IMech Part G: Journal of Aerospace Engineering》《International Journal of Heat and Mass Transfer》《IMech Part A: Journal of Power and Energy》《IMech Part C: Journal of Mechanical Engineering Science》《Chinese Journal of Aeronautics》《Flow, Turbulence and Combustion》《Applied Thermal Engineering》《Applied Energy》《International Journal of Turbo & Jet-Engines》《Aircraft Engineering and Aerospace Technology》《Aerospace Science and Technology》《RSC Adcances》《The International Journal of Advanced Manufacturing Technology》《Journal of Thermal Science》《Journal of Mechanical Science and Technology》《The Scientific World Journal》等.
教育部学位与研究生教育评估中心—学位论文通讯评议专家；
全国大学生节能减排社会实践与科技竞赛网评专家；
国家自然科学基金通讯评审专家。