付衍琛 - 北京航空航天大学 - 航空发动机研究院

个人简介

教育经历 2014.9-2015.9 多伦多大学动力工程及工程热物理公派联合培养 2011.9-2016.12 北京航空航天大学动力工程及工程热物理博士学位博士研究生毕业 2007.9-2011.6 北京科技大学热能与动力工程学士学位大学本科毕业工作经历 2019.1-2019.11 能源与动力工程学院北京航空航天大学 2017.3-2019.1 北京航空航天大学博士后社会兼职 2021.5-2023.5 EI期刊《推进技术》青年编委《International Journal of Heat and Mass Transfer》《Applied Thermal Engineering》《Energy》《Aerospace Science and Technology》《Thermal Science and Engineering Progress》《Journal of Thermal Science》《推进技术》《航空动力学报》等十余种国内外期刊审稿人中国航空学会会员中国航天第三专业信息网综合热管理技术专业委员会委员北航2019级190414班班主任，北航学业导师、北航专属导师荣誉及奖励北京航空航天大学青年拔尖人才支持计划，2022年 GF科学技术进步奖一等奖，2021年，排名第13 中国科协青年人才托举工程，2020年 ***集团科学技术三等奖，2019年，排名第5 北京航空航天大学优秀博士后，2018年北京航空航天大学优秀博士论文，2018年研究生国家奖学金，2015年

研究领域

高超声速组合发动机预冷技术空天动力用高效紧凑换热器高温高压热物性测量极端工况超临界流体流动换热碳氢燃料热氧化结焦及其抑制

近期论文

查看导师最新文章（温馨提示：请注意重名现象，建议点开原文通过作者单位确认）

Experimental study on influences of physical factors to supercritical RP-3 surface and liquid-space thermal oxidation coking Thermal and element analyses for supercritical RP-3 surface coke deposition under stable and vibration conditions Experimental study of flow distribution for aviation kerosene in parallel helical tubes under supercritical pressure Experimental research on convective heat transfer of supercritical hydrocarbon fuel flowing through U-turn tubes Surface coking deposition influences on flow and heat transfer of supercritical hydrocarbon fuel in helical tubes Heat transfer performance of aviation kerosene RP-3 flowing in a vertical helical tube at supercritical pressure Experimental investigation on convective heat transfer of supercritical RP-3 in vertical miniature tubes with various diameters An experimental investigation on heat transfer enhancement of sprayed wire-mesh heat exchangers Thermal and hydraulic performance of a compact plate finned tube air-fuel heat exchanger for aero-engine Buoyancy effects on heat transfer to supercritical pressure hydrocarbon fuel in a horizontal miniature tube Thermal oxidation coking of aviation kerosene RP-3 at supercritical pressure in helical tubes Density measurements of propellant EHF-TU at (3 to 7) MPa supercritical pressures Flow resistance and convective heat transfer performances of airflow through helical-tube bundles Numerical investigation on convective heat transfer of supercritical aviation kerosene in a horizontal tube under hyper gravity conditions Multivariate design and analysis of aircraft HEX under multiple working conditions within flight envelope Frictional resistance of supercritical pressure RP-3 flowing in a vertically downward tube at constant heat fluxes Airside pressure drop characteristics of three analogous serpentine tube heat exchangers considering heat transfer for aero-engine cooling Thermal dynamic and failure research on an air-fuel heat exchanger for aero-engine cooling Vibration effects on heat transfer characteristics of supercritical pressure hydrocarbon fuel in transition and turbulent states