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"Wind Tunnel Model Design with Active Flow Control, for Low Speed Test" (DEAFCON)
Date du début: 1 juil. 2013, Date de fin: 31 déc. 2014,
"The original requirement covered by this DEAFCON proposal was for the detailed design of two low speed half models, with a fully pressure plotted low sweep and high sweep wing respectivelyRemovable and variable Leading Edge, Trailing Edge and Wing Tip devices were to be included, and the main element of innovation and learning for ARA would have been the integration of some form of Active Flow Co ...
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