陈娉婷

个人信息:Personal Information

硕士生导师

招生学科专业:
能源动力 -- 【招收硕士研究生】 -- 能源与动力学院

性别:女

毕业院校:清华大学

学历:清华大学

学位:工学博士学位

所在单位:能源与动力学院

办公地点:明故宫校区10号楼532室

联系方式:cpt09@nuaa.edu.cn

电子邮箱:

扫描关注

个人简介:Personal Profile


个人简介:

陈娉婷,博士,上岗副研究员,硕士生导师。第二批“全国高校黄大年式教师团队”-“动力系统能量高效利用”团队核心成员(团队负责人毛军逵教授)。2021年3月至今在南京航空航天大学能源与动力学院燃烧传热与热能系(205系)工作,主持国家自然科学基金1项,参与多项国家级和省部级项目,近五年在本研究领域顶级国际学术期刊上发表论文30余篇。

教育经历:

2013.8-2019.10    清华大学    动力工程及工程热物理    博士

2017.10-2018.11    明尼苏达大学(University of Minnesota)机械工程    联合培养博士

2009.8-2013.7    清华大学    能源动力系统及自动化     学士

研究方向:

  • 传热传质

  • 航空发动机高效冷却

  • 血流动力学模拟

发表学术论文情况:

[1]. Chen P, Li X, Ren J, et al. Influence of endwall 2D contouring on endwall adiabatic cooling effectiveness and aerodynamic performance[J]. International Journal of Heat and Mass Transfer, 2019, 137: 690-702.

[2]. Chen P, Wang L, Li X, et al. Effect of axial turbine non-axisymmetric endwall contouring on film cooling at different locations[J]. International Journal of Heat and Mass Transfer, 2020

[3]. Chen P, Wang L, Li X, et al. Enhancement of Film Cooling Effectiveness Using Dean Vortices[J]. Journal of Turbomachinery, 2020, 142(1).

[4]. Chen P, Alqefl M, Li X, et al. Cooling effectiveness and aerodynamic performance in a 2D-Contoured endwall passage with different mass flow ratios[J]. International Journal of Thermal Sciences, 2019, 142: 233-246.

[5]. Chen P, Xue Q, Li X, et al. Full coverage film cooling on a non-axisymmetric contoured endwall and the baseline endwall[J]. International Journal of Thermal Sciences, 2020, 158: 106562.

[6]. Chen P, Zhao K, Li X, et al. Full Coverage Effects of Varying Non-axisymmetric Contours of the Turbine Endwall on Aerodynamics and Heat Transfer Aspects: A Sensitivity Analysis Study [J]. International Journal of Thermal Sciences.

[7]. Chen P, Shi W, Li X, Ren J, et al. Using Dean Vortices to Enhance the Film Cooling Performance for Fan Shaped Hole [J]. International Journal of Thermal Sciences.

[8]. Chen P, Wang L, Li X, Ren J, Jiang H. Enhancement of Film Cooling Effectiveness using Dean Vortices [C]. ASME Turbo Expo 2019: Turbomachinery Technical Conference and Exposition,

[9]. Chen P, Gao H, Li X, Ren J, Jiang H. Effects of Endwall 3D Contouring on Film Cooling Effectiveness of Cylindrical Hole Injections at Different Locations on Vane Endwall [C]//ASME Turbo Expo 2018: Turbomachinery Technical Conference and Exposition.

[10]. Chen P, Li X, Ren J, Jiang H. Numerical Investigation on the Effect of Slot Leakage on a NGV with 2D Contoured Endwall: Adiabatic Effectiveness and Aerodynamic Loss[C]//ASME Turbo Expo 2017: Turbomachinery Technical Conference and Exposition

[11]. Chen P, Li X, Ren J, Jiang H. Multi-objective Optimization of Non-axisymmetric Contoured Endwall for Axial Turbines [C]// IGTC 2019: International Gas Turbine Congress 2019 Tokyo

[12].Chen P, Li X, Ren J, Jiang H. Measurement and CFD Prediction of Turbine endwall film cooling [C]// CMFF 2018: Conference on Modelling Fluid Flow, 2018

[13].Chen, P., Li, X., Ren, J., &Jiang, H. Multi-objective optimization of non-axisymmetric contoured endwall for axial turbines[J]. International Journal of Gas Turbine, Propulsion and Power Systems, 2021, 12(1): 1-9.

[14].陈娉婷,李雪英,任静,蒋洪德.燃烧室温度剖面对非轴对称端壁冷却的影响[J].工程热物理学报,2019,40(01):191-197.

[15].陈娉婷,秦晏旻,任静,蒋洪德.带肋通道和气膜冷却交互下的绝热和耦合传热研究[J].工程热物理学报,2016,37(07):1422-1426.

[16].陈娉婷,李雪英,任静,蒋洪德.冲击衬套对于一级静叶气膜孔流量分配和气膜冷却效率的影响[J].工程热物理学报,2015,36(08):1662-1665.

[17].Zeng L, Chen P, Li X, Ren J, Jiang H. Influence of simplifications of blade in gas turbine on film cooling performance[J]. Applied Thermal Engineering, 2018, 128: 877-886.

[18].Qin Y, Chen P, Ren J, Jiang H. Effects of wall curvature and streamwise pressure gradient on film cooling effectiveness[J]. Applied Thermal Engineering, 2016, 107: 776-784.

[19].Shi W, Chen P, Li X, et al. Uncertainty quantification of the effects of squealer tip geometry deviation on aerothermal performance[J]. Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy, 2020: 0957650919898617.

[20].Shi W, Chen P, Li X, et al. Uncertainty Quantification of the Effects of Small Manufacturing Deviations on Film Cooling: A Fan-Shaped Hole[J]. Aerospace, 2019, 6(4): 46.

[21].Shi W, Chen P, Li X, et al. Effects of Squealer Tip Geometry Deviation on Flow Field and Aerodynamic Performance Using Uncertainty Quantification Method and Sensitivity Analysis Method [C]// GPPS-BJ-2019:Global Power and Propulsion

[22].Yang Y, Mao J K, Chen P, et al. Numerical investigation of impingement heat transfer on the crossflow channel with vortex generators[J]. Applied Thermal Engineering, 2022, 201: 117780.

[23].Zhao C, Tu Z, Mao J, Chen P. The design of special woven-preformed structures for the high-performance film cooling with undamaged fibers based on 2.5 D ceramic matrix composites[J]. Composite Structures, 2022, 283: 115114.

[24].Li Z, Chen Y, Chen P, et al. Quantitative evaluation of hemodynamics after partial embolization of brain arteriovenous malformations[J]. Journal of neurointerventional surgery, 2021.

[25].Alqefl, M., Nawathe, K., Chen, P., Zhu, R., Kim, Y, & Simon, T. Aero-thermal Aspects of Film Cooled Nozzle Guide Vane Endwall - Part 1: Aerodynamics[J]. Journal of Turbomachinery, 2021, 1-54.

[26].Alqefl, M., Nawathe, K., Chen, P., Zhu, R., Kim, Y, & Simon, T. Effects of Endwall Film Coolant Flow Rate on Secondary Flows and Coolant Mixing in a First Stage Nozzle Guide Vane[J]. Journal of Turbomachinery, 2021, 143(3):1-54.

[27].Alqefl M. H, Nawathe K, Chen P, Zhu R, Kim Y. W, Simon T. W. A Multi Plenum Superposition Method for Scalar Transport with Application to Endwall Film Cooling [C]// IGTC 2019: International Gas Turbine Congress 2019 Tokyo

[28].Alqefl M. H, Nawathe K, Chen P, Zhu R, Kim Y. W, Simon T. W. AERO-THERMAL ASPECTS OF FILM COOLED NOZZLE GUIDE VANE ENDWALL - PART 1: AERODYNAMICS [C]//ASME Turbo Expo 2020: Turbomachinery Technical Conference and Exposition.

[29].Alqefl M. H, Nawathe K, Chen P, Zhu R, Kim Y. W, Simon T. W. AERO-THERMAL ASPECTS OF FILM COOLED NOZZLE GUIDE VANE ENDWALLS – PART 2 THERMAL MEASUREMENTS [C]//ASME Turbo Expo 2020: Turbomachinery Technical Conference and Exposition.

[30].Alqefl M. H, Nawathe K, Chen P, Zhu R, Kim Y. W, Simon T. W. EFFECTS OF ENDWALL FILM COOLANT FLOW RATE ON SECONDARY FLOWS AND COOLANT MIXING IN A FIRST STAGE NOZZLE GUIDE VANE [C]//ASME Turbo Expo 2020: Turbomachinery Technical Conference and Exposition.

[31].王骁, 李水清, 陈娉婷,等. 环境辐射对固体燃料火焰传播速度的影响[J]. 工程热物理学报, 2013(12):2401-2404.



  • 教育经历Education Background
  • 工作经历Work Experience
  • 研究方向Research Focus
  • 社会兼职Social Affiliations
  • 传热传质
  • 航空发动机高效冷却
  • 血流动力学模拟
    2021.8 至今
    • 《推进技术》青年编委