Aerodynamic Effects of Oversized Tires and Tall Landing Gear on a Small General Aviation Aircraft

1999-01-1592

04/20/1999

Event
General, Corporate & Regional Aviation Meeting & Exposition
Authors Abstract
Content
An experimental investigation was conducted to identify the aerodynamic effects of oversized low-pressure (Tundra) tires and tall landing gear on a Piper Super Cub airplane. Water tunnel and wind tunnel tests were performed using, respectively, a 1/20 scale model and full-scale landing gear and tire components. Force and moment data suggest that larger tires and taller gear most affect the drag and side force. Small trim changes are apparent, but the basic static stability behavior appears unchanged.
Meta TagsDetails
DOI
https://doi.org/10.4271/1999-01-1592
Pages
15
Citation
Miller, L., Thumann, G., and Sanborn, S., "Aerodynamic Effects of Oversized Tires and Tall Landing Gear on a Small General Aviation Aircraft," SAE Technical Paper 1999-01-1592, 1999, https://doi.org/10.4271/1999-01-1592.
Additional Details
Publisher
Published
Apr 20, 1999
Product Code
1999-01-1592
Content Type
Technical Paper
Language
English