兵工自动化2012，Vol.31Issue(1)：37-41,5.DOI:10.3969/j.issn.1006-1576.2012.01.012
固体燃料超燃冲压发动机燃烧室的数值仿真
Numerical Simulation of a Solid Fuel Scramjet Combustors
杨明 1孙波1
作者信息
- 1. 南京理工大学航空宇航系,南京210094
- 折叠
摘要
Abstract
Based on a solid fuel scramjet experiment date, A CFD software is used in the numerical simulation respectively about scramjet combustor of the initial condition and the burning flow after the launch. Given the import boundary of PMMA fuel according to user defined function way. Numerical simulation results indicate that the flow field characteristics in combustor accord with theoretical analysis; it has certain different about the fuel regression rate on the surface of the solid fuel in combustor compare with experimental measurement, but the whole burning face's distribution curve of fuel regression rate along the axial is approximate with the experimental value; The pressure distribution near fuel surface along the axial is satisfying agreement with the experimental data. The results of the study show that the numerical model established is reasonable and have some reference value for the theory research of solid fuel scramjet.关键词
超燃冲压发动机/数值模拟/流场特性/燃料退移速率Key words
scramjet/ numerical simulation/ flow field characteristics/ fuel regression rat分类
信息技术与安全科学引用本文复制引用
杨明,孙波..固体燃料超燃冲压发动机燃烧室的数值仿真[J].兵工自动化,2012,31(1):37-41,5.
