Analytical Simulation of Landing Gear Dynamics for Aircraft Design and Analysis

710401

02/01/1971

Event
National Business Aircraft Meeting and Engineering Display
Authors Abstract
Content
This paper presents an analysis of a nonlinear landing gear mounted on a flexible airplane equipped with external stores and tip tanks. Interaction effects of the flexible airplane with the gear are included. The method of treating the strut lockup-breakout phenomena is an improvement over previous work. Test results are presented from a full scale test of an airplane supported on displacement controlled hydraulic actuators, which simulated taxiing over discrete runway bumps. The analytical method was applied to several design problems which are also discussed.
Meta TagsDetails
DOI
https://doi.org/10.4271/710401
Pages
9
Citation
Furnish, J., and Anders, D., "Analytical Simulation of Landing Gear Dynamics for Aircraft Design and Analysis," SAE Technical Paper 710401, 1971, https://doi.org/10.4271/710401.
Additional Details
Publisher
Published
Feb 1, 1971
Product Code
710401
Content Type
Technical Paper
Language
English