个人简历

教育经历
2002.4 -- 2005.6南京航空航天大学 航空宇航推进理论与工程 博士研究生毕业 工学博士学位
1989.9 -- 1992.3南京航空航天大学 工程热物理 硕士研究生毕业 工学硕士学位
1985.9 -- 1989.7南京航空航天大学 航空发动机 大学本科毕业 工学学士学位
工作经历
2005.6 -- 至今南京航空航天大学
1992.4 -- 2002.3金城集团
专利
[1] 一种蒸发式组合火焰稳定器：ZL201811597557.2[p].
[2] 一种旋流离心燃烧试验装置：ZL201810059210.6[p].
[3] 一种集导流和旋流一体化的叶栅式装置及燃烧室：ZL201810059210.6[p].
[4] 基于进口旋流整流支板调节燃烧区的燃烧室及其专用支板：ZL201810014344.6[p].
[5] 一种基于外凹腔的旋流加力燃烧室：ZL201711477824.8[p].
[6] 一种可调节凹腔涡区结构的组合火焰稳定器及其工作方法：ZL201910019370.2[p].
[7] 一种超燃冲压发动机燃烧室中心点火机构：ZL201410595815.9[p].
[8] 一种蒸发式火焰稳定器：ZL201410231619.3[p].
[9] 涡轮基组合循环发动机超级燃烧室：ZL201410231348.1[p].
[10] 带有新型冷却结构一体化设计的火焰稳定器：ZL201610107755.0[p].
[11] 一种带有凸台扰流结构的火焰稳定器：ZL201510850703.8[p].
科研项目
[1] 多涵道加力燃烧室高效燃烧组织技术研究
[2] XXX技术验证机多模态冲压燃烧室一体化稳定器油雾分布特性
[3] XXX技术验证机多模态冲压燃烧室外凹腔火焰稳定器部件性能试验研究
[4] XXX技术验证机多模态冲压燃烧室宽范围火焰稳定器技术研究
[5] 小流量燃油喷嘴热防护设计技术研究
[6] 基于多管PDE爆震推进的关键技术研究
授课信息
燃气轮机原理与构造 /2020-2021 /秋学期 /48课时 /0.0学分 /02203110
[7] 超级燃烧室掺混技术研究
[8] 低流阻气动强化扰流起爆方法研究
[9] 超级燃烧室模型件设计及性能验证
[10] 超级燃烧室火焰稳定及供油技术研究
[11] 稳定喷油一体化火焰稳定器设计及试验研究
[12] 声能喷嘴冷热态性能分析与研究
[13] T**XX技术验证机多模态冲压燃烧室第二轮火焰稳定器模型试验研究
[14] 项目开发
[15] 项目开发

研究领域

""

近期论文

[1] Influence of struts on cavity at subsonic speeds: Flow characteristics[J].Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering,2019,162:56-65
[2] Effects of a jet turbulator upon flame acceleration in a detonation tube.Applied Thermal Engineering,2016,115:33-40
[3] Experimental and numerical study on fuel distribution and flame expansion of the enhanced flame holding devices[J].Energy,2021,203
[4] Influence of injection scheme on flame characteristics in partially premixed combustion[J].Energy,2021,205
[5] Influence of injection scheme on flame characteristics in partially premixed combustion[J].Energy,2021,209
[6] Experimental and numerical study on thermodynamic characteristics in a Z-shaped evaporating pilot-flameholder[J].Acta Astronautica,2020,162:56-65
[7] Influence of air-entraining intensity on the afterburner ignition, flame-holding and combustion characteristics[J].Aerospace Science and Technology,106
[8] Effect of preheated fuel supply by gas reflux on thermodynamic characteristics in a cavity-based integrated combustor[J].Aerospace Science and Technology,108
[9] Ignition characteristics in evaporating Z-shaped pilot flame-holder[J].Journal of Aerospace Power,2020,35(7):1457-1465
[10] Fuel distribution and evaporation characteristics downstream of an integrated flameholder[J].Fuel,2020,266
[11] Effect of air-assistant on ignition and flame-holding characteristics in a cavity-strut based combustor[J].Applied Energy,2020,106
[12] 范育新,范育新,范育新等.Influence of parameters on flame expansion in a high-speed flow: Experimental and numerical study.Journal of Power and Energy,2019
[13] 范育新,范育新,范育新等.Analysis of flow resistance and combustion characteristics in the combined application of step and strut: Experimental study.Aerospace Science and Technology,2019
[14] 范育新,Zhai, Wen-Hui,Zhai, Wen-Hui等.Flow Characteristics of TBCC Swirled Combustion in Turbofan Mode.Tuijin Jishu,2019
[15] 范育新,,等.Experimental and numerical study on thermodynamic characteristics in a Z-shaped evaporating pilot-flameholder.Acta Astronaut,2019