SAE AIR 4358 : 2012

Table of Contents

FOREWORD
1. SCOPE
2. APPLICABLE DOCUMENTS
3. ORIGIN OF CORNERING FORCES
4. EFFECT OF LANDING GEAR PARAMETERS ON
   FREE-SWIVELING STEERING FORCES
5. DESIGN CONSIDERATIONS
6. TESTING TECHNIQUES
7. KEY WORDS

Abstract

Provides the origin of cornering forces generated by tilted, free-swiveling nose gears; the effect of various landing gear parameters on the measured cornering forces; and a method of towing aircraft to measure the resulting steering forces.

General Product Information

Published
Document Type	Standard
Status	Current
Publisher	SAE International
Pages
ISBN
Committee	A-5