Stability analysis of boundary-layer transition using accurate velocity profiles obtained by an advanced LES
Laminar-turbulent transition of the boundary layer is discussed from a view point of ac- curacy of the computational uid dynamics. When highly accurate velocity profiles are used for stability analysis, curve of N factor of the e N method becomes apart from the curve of conventional laminar- ow computation. Furthermore, N value does not reach sufficient large value even in the situation that laminar-turbulent transition may occur. With the excellent computation, usefulness of the accurate velocity profiles for the transition issue is sought.
boundary layer transition the e N method large eddy simulation
T.Atobe T.Kurotaki T.Sumi J.Hiyama
Institute of Aerospace Technology, Japan Aerospace Exploration Agency, Chofu Tokyo, 182-8522 Japan Sanko Aerospace Dept.Co., Ltd., Shinjuku Tokyo, 169-0075 Japan
国际会议
The Fifth International Conference on Fluid Mechanics(第五届国际流体力学会议)
上海
英文
2007-08-15（万方平台首次上网日期，不代表论文的发表时间）