Abstract: Wings experiencing large flow disturbances often experience massive flow separation resulting in shear layers and the formation of strong vortices. These vortices typically lead to large ...
The dorsal S-duct inlet of a HALE blended wing body UAV faces complex unsteady disturbances during operation. This study ...
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Unfortunately, this book can't be printed from the OpenBook. Visit NAP.edu/10766 to get more information about this book, to buy it in print, or to download it as a free PDF.