The Generation of Tire Cornering Forces in Aircraft with a Free-Swiveling Nose Gear

851939

10/01/1985

Event
Aerospace Technology Conference and Exposition
Authors Abstract
Content
Various conditions can cause an aircraft to assume a roll or tilt angle on the runway, causing the nose tire(s) to produce significant uncommanded cornering forces if the nose gear is free to swivel. An experimental investigation was conducted using a unique towing system to measure the cornering forces generated by a tilted aircraft tire. The effects of various parameters on these cornering forces including tilt angle, trail, rake angle, tire inflation pressure, vertical load, and twin-tire configuration were evaluated. Corotating twin-tires produced the most severe cornering forces due to tilt angle. A discussion of certain design and operational considerations is included.
Meta TagsDetails
DOI
https://doi.org/10.4271/851939
Pages
12
Citation
Daugherty, R., and Stubbs, S., "The Generation of Tire Cornering Forces in Aircraft with a Free-Swiveling Nose Gear," SAE Technical Paper 851939, 1985, https://doi.org/10.4271/851939.
Additional Details
Publisher
Published
Oct 1, 1985
Product Code
851939
Content Type
Technical Paper
Language
English