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Large eddy simulation of shock boundary layer interaction in a transonic internal flow

Moroianu, Dragos LU ; Caraeni, Doru LU and Fuchs, Laszlo LU (2005) 43rd AIAA Aerospace Sciences Meeting and Exhibit p.6533-6542
Abstract
The paper presents a study of the dynamics of non-stationary shock wave and its interaction with the boundary layer in a transonic flow inside a channel with a bump. The turbulent flow is handled using Large Eddy Simulations (LES). The computations are done with the recently developed multidimensional upwind scheme and with two other commercial codes. The aim is to improve the understanding of the mechanism of shock wave dynamics, viscous/inviscid and the presence of solution hysteresis. The numerical results are compared to available experimental data.
Please use this url to cite or link to this publication:
author
; and
organization
publishing date
type
Chapter in Book/Report/Conference proceeding
publication status
published
subject
keywords
Large eddy simulation, Shock wave dynamics, Shock boundary layers
host publication
43rd AIAA Aerospace Sciences Meeting and Exhibit - Meeting Papers
pages
6533 - 6542
publisher
American Institute of Aeronautics and Astronautics
conference name
43rd AIAA Aerospace Sciences Meeting and Exhibit
conference location
Reno, NV, United States
conference dates
2005-01-10 - 2005-01-13
external identifiers
  • scopus:30744432656
language
English
LU publication?
yes
id
663c2ee6-8f14-472c-84d0-0c5622554b2a (old id 616047)
alternative location
http://pdf.aiaa.org/preview/CDReadyMASM05_666/PV2005_312.pdf
date added to LUP
2016-04-04 11:19:51
date last changed
2020-01-12 21:23:59
@inproceedings{663c2ee6-8f14-472c-84d0-0c5622554b2a,
  abstract     = {The paper presents a study of the dynamics of non-stationary shock wave and its interaction with the boundary layer in a transonic flow inside a channel with a bump. The turbulent flow is handled using Large Eddy Simulations (LES). The computations are done with the recently developed multidimensional upwind scheme and with two other commercial codes. The aim is to improve the understanding of the mechanism of shock wave dynamics, viscous/inviscid and the presence of solution hysteresis. The numerical results are compared to available experimental data.},
  author       = {Moroianu, Dragos and Caraeni, Doru and Fuchs, Laszlo},
  booktitle    = {43rd AIAA Aerospace Sciences Meeting and Exhibit - Meeting Papers},
  language     = {eng},
  pages        = {6533--6542},
  publisher    = {American Institute of Aeronautics and Astronautics},
  title        = {Large eddy simulation of shock boundary layer interaction in a transonic internal flow},
  url          = {http://pdf.aiaa.org/preview/CDReadyMASM05_666/PV2005_312.pdf},
  year         = {2005},
}