上海航天（中英文）2025，Vol.42Issue(2)：194-202,9.DOI:10.19328/j.cnki.2096-8655.2025.02.019
考虑多种物理效应的轨控喷流数值计算研究
Numerical Simulation of Orbit-controlled Jet Considering Multi-physical Effects
万钊 1华如豪 1陈琦 1江定武 1王新光1
作者信息
- 1. 中国空气动力研究与发展中心 计算空气动力研究所,四川 绵阳 621000
- 折叠
摘要
Abstract
The prediction accuracy of orbit-controlled jet is the key technology of high-speed interception weapons.Currently,there are scarce studies on the jet interaction at high altitudes and large Mach numbers,and the law of influence of various physical effects on the jet interaction during high-speed flight in this airspace is not systematic enough.By solving the three-dimensional chemical non-equilibrium Navier-Stokes equation with slip boundary conditions,the influence of the high-temperature thermochemical non-equilibrium effect,gas secondary combustion effect,and rarefied gas effect on the orbit-controlled jet interaction is analyzed,and the influence of various physical effects on the aerodynamic characteristics of the orbit-controlled jet interaction under different flow conditions is obtained.The results indicate that the high-temperature dissociation reaction of the incoming air and gas components is the main factor accounting for the difference between the cold air and hot gas at high altitudes and large Mach numbers,and the influence degree decreases when the altitude increases while increases when the Mach number increases.The influence of the rarefied gas effect on the interaction aerodynamic force/moment of the overall jet is minor.关键词
高温真实气体效应/稀薄气体效应/热喷干扰/数值模拟Key words
high-temperature real gas effect/rarefied gas effect/hot-gas jet interaction/numerical simulation引用本文复制引用
万钊,华如豪,陈琦,江定武,王新光..考虑多种物理效应的轨控喷流数值计算研究[J].上海航天（中英文）,2025,42(2):194-202,9.
