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Instability analysis and drag coefficient prediction on a swept RAE2822 wing with constant lift coef
[期刊论文] 作者：Zhenrong JING,Zhangfeng HUANG,,
来源：Chinese Journal of Aeronautics 年份：2017
Swept wing is widely used in civil aircraft,whose airfoil is chosen,designed and optimized to increase the cruise speed and decrease the drag coefficient.The pa...
[会议论文] 作者：Zhangfeng Huang,Xuesong Wu,
来源：7th International Conference on Fluid Mechamics(ICFM7)(第七届国际 年份：2015
This paper presents a local,simple and non-perturbative approach to spatial instability of three-dimensional compressible boundary layers,which takes into accou...
[期刊论文] 作者：ZhangFeng Huang (1) (2), Heng,
来源：中国科学：物理学、力学、天文学英文版 年份：2008
The inflow conditions for spatial direct numerical simulation(SDNS) of turbulent boundary layers should reflect the characteristics of upstream turbulence,which...
[期刊论文] 作者：Shaoxian Ma,Yi Duan,Zhangfeng Huang,Shiyong Yao,
来源：中国物理B（英文版） 年份：2021
The nonlinear parabolized stability equations (NPSEs) approach is widely used to study the evolution of disturbances in hypersonic boundary layers owing to its...
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