Three-axis control of tailless aircraft using fluidic actuators: MAGMA case study (2021)
Attributed to:
Control of spanwise flow induced separation on swept low aspect ratio wings to improve controllability
funded by
EPSRC
Abstract
No abstract provided
Bibliographic Information
Digital Object Identifier: http://dx.doi.org/10.2514/6.2021-2530
Publication URI: http://dx.doi.org/10.2514/6.2021-2530
Type: Conference/Paper/Proceeding/Abstract