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.
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Matlab, text file editor
Keywords
shock control bumps, SCB, flow control, sweep, swept wing, drag, computational fluid dynamics
Publisher
University of Cambridge
Sponsorship
EPSRC DTA