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Research Data Supporting "Adapting Three-Dimensional Shock Control Bumps to Swept Flows"


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Description

CFD simulations of infinite-swept wings with shock control bumps; parametric study Matlab files (.mat) contain a set of reduced data, obtained from batch post-processing of raw simulation files. Further information on contents and how to access file contents are contained in readme text files within data folders.

Version

Software / Usage instructions

Matlab, text file editor

Publisher

University of Cambridge

Rights and licensing

Except where otherwised noted, this item's license is described as Attribution-NonCommercial 4.0 International
Sponsorship
EPSRC DTA

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