Shock-Wave/Boundary-Layer Interaction at M=1.5 Dataset

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]


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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

Item Type: Dataset
Digital Object Identifier (DOI): doi:10.5258/SOTON/381784
Related URLs:
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
ePrint ID: 381784
Date :
Date Event
15 January 2016Published
Date Deposited: 15 Jan 2016 17:24
Last Modified: 09 Jun 2017 13:16
Further Information:Google Scholar

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