Hoverfoil™ Design and Testing

F-0078-2022-1282

5/10/2022

Authors
Abstract
Content

The Hoverfoil(TM) is an engineered wing-in-ground effect airfoil that can maintain lift while at zero forward velocity. This is done by use of internally routed duct work that channels airflow through the airfoil to the underside, to create an area of high pressure on the bottom of the Hoverfoil(TM). The airfoil shape (excluding ductwork) utilized a NACA 8308 airfoil. A combination of computational fluid dynamic (CFD) models and 3D scale prototyping have been used to study the feasibility of the project. The CFD model has proven the initial idea as feasible, however the implementation of the scale prototype needs to overcome some barriers to complete testing.

Meta TagsDetails
DOI
https://doi.org/10.4050/F-0078-2022-1282
Citation
Echols, K. and Petersen, R., "Hoverfoil™ Design and Testing," Vertical Flight Society 78th Annual Forum and Technology Display, Fort Worth, Texas, May 10, 2022, https://doi.org/10.4050/F-0078-2022-1282.
Additional Details
Publisher
Published
5/10/2022
Product Code
F-0078-2022-1282
Content Type
Technical Paper
Language
English