Affiliation of Author(s):航空学院
Journal:MODERN PHYSICS LETTERS B
Key Words:Aerodynamic heating ablation effects structure conduction hypersonic vehicles
Abstract:A numerical method of aerodynamic heating with material thermal ablation effects for hypersonic half-sphere is presented. A surface material ablation model is provided to analyze the ablation effects on aero-thermal properties and structural heat conduction for thermal protection system (TPS) of hypersonic vehicles. To demonstrate its capability, applications for thermal analysis of hypersonic vehicles using carbonaceous ceramic ablators are performed and discussed. The numerical results show the high efficiency and validation of the method developed in thermal characteristics analysis of hypersonic aerodynamic heating.
ISSN No.:0217-9849
Translation or Not:no
Date of Publication:2018-05-10
Co-author:Li, Jia-Wei,Zhao, Fa-Ming,Fan, Xiao-Feng
Correspondence Author:WANG Jiangfeng
Professor
Supervisor of Doctorate Candidates
Gender:Male
Alma Mater:南京航空航天大学； Université Pierre et Marie Curie
Education Level:法国巴黎第六大学
Degree:Doctoral Degree in Engineering
School/Department:College of Aerospace Engineering
Discipline:Fluid Mechanics. Fluid Mechanics
Business Address:本部流体楼（C12）- 301室
Contact Information:wangjf@nuaa.edu.cn
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