Numerical Simulation of Hypersonic Viscous Flow around an Aerospace Plane

摘要：

This paper deals with an aerospace plane with notail-fuselages and leaping triangle wing tip similar to HERMES of France and HOPE of Japan. Numerical simulations were performed for Mach numbers of 4.96 (Re=3.1×107/m) at angles of attack from-5 deg to 20 deg using the Multi-block Structure NS solver. Comparisons between the predicted aerodynamic characteristics and wind tunnel data verify the reliability of the numerical method used for simulating viscous flow around the aerospace plane.

关键词： aerospace plane hypersonic flow aerodynamic characteristics numerical simulation

作者: LiuJieping ChenHewu Zhang Weimin

作者单位: China Academy of Aerospace Aerodynamics, Beijing P.O. Box 7201-56, Beijing, P.R. China, 100074

会议类型: 国际会议

会议名称: The 8th Sino-Russia High-speed Flow Conference(第八届中俄高超声速流体力学研讨会)

会议地点: 上海

会议语种:英文

页码: 8-13

在线出版日期: 2011-11-21（万方平台首次上网日期，不代表论文的发表时间）