摘要
本文应用有限体积法求解Ｅｕｌｅｒ方程，数值模拟翼身组合体大攻角、跨声速绕流。成功地模拟了机身体涡、机翼脱体涡、翼尖侧缘涡的形成、发展及其相互间的干扰。
A finite volume scheme is used to solve Euler equations in order to simulate transonic high-angle-of attack flow over a wing-body combination. Successfully obtained the eyolution of body and wing vortices and their mutual interaction.
出处
《空气动力学学报》
CSCD
北大核心
1996年第2期205-209,共5页
Acta Aerodynamica Sinica
关键词
有限体积法
翼身组合体
体涡
翼涡
finite-volume scheme, wing-body combination, body vortex, wing vortex.
