Large eddy simulation of shock boundary layer interaction in a transonic internal flow
(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:
https://lup.lub.lu.se/record/616047
- author
- Moroianu, Dragos LU ; Caraeni, Doru LU and Fuchs, Laszlo LU
- organization
- publishing date
- 2005
- 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
- 2022-01-29 21:41:47
@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}}, keywords = {{Large eddy simulation; Shock wave dynamics; Shock boundary layers}}, 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}}, }