Roll Control of Low-Aspect-Ratio Wings Using Articulated Winglet Control Surfaces
Crossref DOI link: https://doi.org/10.2514/1.C034704
Published Print: 2019-03
Update policy: https://doi.org/10.2514/aiaa_crossmarkpolicy
O’Donnell, Richard
Mohseni, Kamran
Funding for this research was provided by:
Air Force Office of Scientific Research
Accepted Manuscript valid from 2020-01-29
Publication History
Received: 2017-08-14
Revised: 2018-04-13
Accepted: 2018-11-01
Published: 2019-01-29