Implicit LES for Supersonic Microramp Vortex Generator: New Discoveries and New Mechanisms

This paper serves as a summary of our recent work on LES for supersonic MVG. An implicitly implemented large eddy simulation (ILES) by using the fifth-order WENO scheme is applied to study the flow around the microramp vortex generator (MVG) at Mach 2.5 and Re⁡θ=1440. A number of new discoveries on...

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Main Authors: Qin Li, Chaoqun Liu
Format: Article
Language:English
Published: Hindawi Limited 2011-01-01
Series:Modelling and Simulation in Engineering
Online Access:http://dx.doi.org/10.1155/2011/934982
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spelling doaj-d2acafeae12643c49407a5c5af4eaaa72020-11-24T22:24:32ZengHindawi LimitedModelling and Simulation in Engineering1687-55911687-56052011-01-01201110.1155/2011/934982934982Implicit LES for Supersonic Microramp Vortex Generator: New Discoveries and New MechanismsQin Li0Chaoqun Liu1Math Department, University of Texas at Arlington, 411 S. Nedderman Drive, Arlington, TX 76019-0408, USAMath Department, University of Texas at Arlington, 411 S. Nedderman Drive, Arlington, TX 76019-0408, USAThis paper serves as a summary of our recent work on LES for supersonic MVG. An implicitly implemented large eddy simulation (ILES) by using the fifth-order WENO scheme is applied to study the flow around the microramp vortex generator (MVG) at Mach 2.5 and Re⁡θ=1440. A number of new discoveries on the flow around supersonic MVG have been made including spiral points, surface separation topology, source of the momentum deficit, inflection surface, Kelvin-Helmholtz instability, vortex ring generation, ring-shock interaction, 3D recompression shock structure, and influence of MVG decline angles. Most of the new discoveries, which were made in 2009, were confirmed by experiment conducted by the UTA experimental team in 2010. A new 5-pair-vortex-tube model near the MVG is given based on the ILES observation. The vortex ring-shock interaction is found as the new mechanism of the reduction of the separation zone induced by the shock-boundary layer interaction.http://dx.doi.org/10.1155/2011/934982
collection DOAJ
language English
format Article
sources DOAJ
author Qin Li
Chaoqun Liu
spellingShingle Qin Li
Chaoqun Liu
Implicit LES for Supersonic Microramp Vortex Generator: New Discoveries and New Mechanisms
Modelling and Simulation in Engineering
author_facet Qin Li
Chaoqun Liu
author_sort Qin Li
title Implicit LES for Supersonic Microramp Vortex Generator: New Discoveries and New Mechanisms
title_short Implicit LES for Supersonic Microramp Vortex Generator: New Discoveries and New Mechanisms
title_full Implicit LES for Supersonic Microramp Vortex Generator: New Discoveries and New Mechanisms
title_fullStr Implicit LES for Supersonic Microramp Vortex Generator: New Discoveries and New Mechanisms
title_full_unstemmed Implicit LES for Supersonic Microramp Vortex Generator: New Discoveries and New Mechanisms
title_sort implicit les for supersonic microramp vortex generator: new discoveries and new mechanisms
publisher Hindawi Limited
series Modelling and Simulation in Engineering
issn 1687-5591
1687-5605
publishDate 2011-01-01
description This paper serves as a summary of our recent work on LES for supersonic MVG. An implicitly implemented large eddy simulation (ILES) by using the fifth-order WENO scheme is applied to study the flow around the microramp vortex generator (MVG) at Mach 2.5 and Re⁡θ=1440. A number of new discoveries on the flow around supersonic MVG have been made including spiral points, surface separation topology, source of the momentum deficit, inflection surface, Kelvin-Helmholtz instability, vortex ring generation, ring-shock interaction, 3D recompression shock structure, and influence of MVG decline angles. Most of the new discoveries, which were made in 2009, were confirmed by experiment conducted by the UTA experimental team in 2010. A new 5-pair-vortex-tube model near the MVG is given based on the ILES observation. The vortex ring-shock interaction is found as the new mechanism of the reduction of the separation zone induced by the shock-boundary layer interaction.
url http://dx.doi.org/10.1155/2011/934982
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AT chaoqunliu implicitlesforsupersonicmicrorampvortexgeneratornewdiscoveriesandnewmechanisms
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