摘要
为高超音速飞行的弹翼建立了气动加热及烧蚀的数学模型 ,并编制了计算软件 ,用于模拟高超音速穿甲弹弹翼前缘的瞬时热效应 .所采用的理论、方法及计算结果对以后进行高超音速弹箭的研究有一定的参考价值 .
The aerodynamic heating and ablation model of hypersonic projectile wing is established. The software is organized to simulate the transient thermal response of the front region of projectile wing such as those launched by electromagnetic chemical guns. The theory, method and results presented in the paper are available for the study of hypersonic projectiles in the future.
出处
《弹道学报》
EI
CSCD
北大核心
2001年第2期41-44,共4页
Journal of Ballistics
关键词
弹翼
高超音速
气动加热
烧蚀
projectile wing, hypersonic, aerodynamic heating, ablation