Frontiers in Aerospace Science

Volume: 2

Turbulent Inflow and LES Validation

Author(s): Chaoqun Liu, Qin Li, Yonghua Yan, Yong Yang, Guang Yang and Xiangrui Dong

Pp: 177-185 (9)

DOI: 10.2174/9781681085975117020006

* (Excluding Mailing and Handling)


In this chapter, a high order direct numerical simulation (DNS) is applied to generate fully developed turbulent inflow. The fully developed inflow was taken from a case of DNS for flow transition. The inflow condition is carefully checked with the velocity profile and ratio of boundary layer thickness, ensuring that it is a fully developed turbulent flow in order to compare with the wind tunnel test.

Keywords: Boundary layer thickness, Fully developed turbulent flow, High order DNS, Velocity profile.

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