Shock-Wave/Boundary-Layer Interaction at M=1.5 Dataset
Shock-Wave/Boundary-Layer Interaction at M=1.5 Dataset
A selection of DNS flow cases examined inSansica, A. (2015), "Stability and Unsteadiness of transitional Shock-Wave/Boundary-Layer Interactions in Supersonic Flows". PhD thesis, University of Southamptonare made available to the public.The dataset can be requested via http://library.soton.ac.uk/datarequest
Shock-wave/boundary-layer interaction, dataset, supersonic boundary-layer, transition to turbulence, linear/nonlinear stability, compressible flows
University of Southampton
SANSICA, ANDREA
f9d20b04-ef9c-4f72-9e14-f9e6d2e84ab5
Sandham, Neil
0024d8cd-c788-4811-a470-57934fbdcf97
Hu, Zhiwei
dd985844-1e6b-44ba-9e1d-fa57c6c88d65
SANSICA, ANDREA
f9d20b04-ef9c-4f72-9e14-f9e6d2e84ab5
Sandham, Neil
0024d8cd-c788-4811-a470-57934fbdcf97
Hu, Zhiwei
dd985844-1e6b-44ba-9e1d-fa57c6c88d65
SANSICA, ANDREA, Sandham, Neil and Hu, Zhiwei
(2016)
Shock-Wave/Boundary-Layer Interaction at M=1.5 Dataset.
University of Southampton
doi:10.5258/SOTON/381784
[Dataset]
Abstract
A selection of DNS flow cases examined inSansica, A. (2015), "Stability and Unsteadiness of transitional Shock-Wave/Boundary-Layer Interactions in Supersonic Flows". PhD thesis, University of Southamptonare made available to the public.The dataset can be requested via http://library.soton.ac.uk/datarequest
Text
Dataset description
- Dataset
More information
Published date: 15 January 2016
Keywords:
Shock-wave/boundary-layer interaction, dataset, supersonic boundary-layer, transition to turbulence, linear/nonlinear stability, compressible flows
Organisations:
Aerodynamics & Flight Mechanics Group, Aeronautics, Astronautics & Comp. Eng
Identifiers
Local EPrints ID: 381784
URI: http://eprints.soton.ac.uk/id/eprint/381784
PURE UUID: 616cfae8-be6a-46aa-9521-c24e42133ba5
Catalogue record
Date deposited: 15 Jan 2016 17:24
Last modified: 25 Oct 2019 00:37
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Contributors
Creator:
ANDREA SANSICA
Creator:
Neil Sandham
University divisions
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