Abstract
In the paper, dynamic characteristics of aircraft wheels are analyzed through building mathematical model of vertical force, longitudinal resistance force, and lateral force of aircraft wheels. Simulation software of force properties of aircraft wheels is developed based on a certain type of aircraft. Finally with the software loaded into an engineering simulator and tested, the accuracy and effectiveness of the software are evaluated according to simulation results.
Published Version
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have