Numerical Study of Blunt Leading Edge Separation on a 53 Degree Swept Diamond Wing (STO AVT-183) Using the Edge and Cobalt Flow Solvers (AIAA 2015-0290)
Aerospace sciences meeting
2015-01-01
33 pages
Conference paper
English
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British Library Conference Proceedings | 2015
|British Library Conference Proceedings | 2015
|Numerical Analysis of Incipient Separation on 53° Swept Diamond Wing (AIAA 2015-0288)
British Library Conference Proceedings | 2015
|