Vertical Takeoff and Landing Aircraft, Vertical Takeoff and Landing Ground Effects

Authors Abstract
Content
The ground-effect problems of loss of thrust and fountain-effect instabilities are quantified. Experiments to control and augment ground-effect lift and stability are presented, including jet momentum reflection and fountain redirection using various types of internal and external underbody ventral strakes. By strategically designing the vertical takeoff and landing (VTOL) ventral surface, reflection of the impinging fountain momentum is possible so that instead of losing 10% thrust while in ground-effect, remarkably, thrust is augmented 10% or more to a considerable height above the ground, in addition to stabilizing random pitch and roll moments caused by fountain instability.
Meta TagsDetails
DOI
https://doi.org/10.4271/01-14-01-0001
Pages
12
Citation
Greene, P., "Vertical Takeoff and Landing Aircraft, Vertical Takeoff and Landing Ground Effects," SAE Int. J. Aerosp. 14(1):33-43, 2021, https://doi.org/10.4271/01-14-01-0001.
Additional Details
Publisher
Published
Aug 20, 2020
Product Code
01-14-01-0001
Content Type
Journal Article
Language
English