Frontiers in Aerospace Science

Frontiers in Aerospace Science

Volume: 2

High Order Large Eddy Simulation for Shock-Boundary Layer Interaction Control by a Micro-ramp Vortex Generator

Indexed in: EBSCO.

This volume presents an implicitly implemented large eddy simulation (ILES) by using the fifth order bandwidth-optimized WENO scheme. The chosen method is applied to make comprehensive studies on ...
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Governing Equations

Pp. 38-87 (50)

Chaoqun Liu, Qin Li, Yonghua Yan, Yong Yang, Guang Yang and Xiangrui Dong


In this chapter, the dimensional and non-dimensional 3-D time-dependent Navier-Stokes equations in curvilinear coordinates are given in details. The flux splitting scheme and non-reflecting boundary conditions are discussed and provided.


Curvilinear coordinates, Flux splitting, Navier-Stokes equations, Non-reflecting boundary conditions.


Center for Numerical Simulation and Modeling, Department of Mathematics, University of Texas at Arlington, Arlington, Texas 76019, TX, USA.