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

Series Title: Frontiers in Aerospace Science

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

Volume 2

eBook: US $39 Special Offer (PDF + Printed Copy): US $191
Printed Copy: US $171
Library License: US $156
ISSN: 2468-4716 (Print)
ISSN: 2468-4724 (Online)
ISBN: 978-1-68108-598-2 (Print)
ISBN: 978-1-68108-597-5 (Online)
Year of Publication: 2017
DOI: 10.2174/97816810859751170201


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 ramp flows with and without control at Mach 2.5 and Re=5760. Flow control in the form of microramp vortex generators (MVG) is applied. The results show that a MVG can distinctly reduce the separation zone at the ramp corner and lower the boundary layer shape factor under the condition of the computation. A series of new findings about the MVG-ramp flow are obtained, including the structures of the surface pressure, the three-dimensional structures of the re-compression shock waves, the complete surface separation pattern, the momentum deficit and a new secondary vortex system.

A new mechanism of shock-boundary layer interaction control by MVG associated with a series of vortex rings is also presented. Vortex rings strongly interact with air flow and play an important role in the separation zone reduction. Additionally, readers will learn about the governing equation, boundary condition, high quality grid generation, high order shock capturing scheme and DNS inflow condition in detail. This volume will, therefore, serve as a useful reference for aerospace researchers using LES methods to study shock boundary layer interaction and supersonic flow control.


.Advanced Control of Flight Vehicle Maneuver and Operation.
.Conceptual Design of Green Transport Airplanes.
.Aerospace Structures and Materials.