Research Data Supporting "Adapting Three-Dimensional Shock Control Bumps to Swept Flows"
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下载链接：
https://www.repository.cam.ac.uk/handle/1810/256472
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资源简介：
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.
提供机构：
Apollo - University of Cambridge Repository
创建时间：
2016-06-24
