This SAE Aerospace Recommended Practice (ARP) is to provide a recommended minimum laboratory roll performance for main landing gear aircraft wheels without tires installed and applies to both bolted and lock-ring wheel designs for FAA Part 25 and military aircraft main wheels (not required for any nose wheels or main wheels on FAA Part 23, 27 or 29 applications). This document is intended to provide recommended practice for aircraft wheel roll on rim design criteria and validation test. This revision C is an update to revision B and incorporates an updated reference section.
Wheel Roll on Rim Criteria for Aircraft Applications
2019-02-15
Conference paper
English
Wheel Roll on Rim Criteria for Aircraft Application
SAE Technical Papers | 2000
Wheel Roll on Rim Criteria for Aircraft Application
SAE Technical Papers | 2010
WHEEL ROLL ON RIM CRITERIA FOR AIRCRAFT APPLICATION
SAE Technical Papers | 1994
Wheel roll on rim criteria for aircraft application
TIBKAT | 2000
Roll-performance criteria for high augmented aircraft
AIAA | 1991
|