Abstract
The objective of this paper is to address finite element modeling for dynamics and its applications to aircraft landing and braking systems. The components of the system in the example model include the entire landing gear, wheels, brakes, and tires. The use of finite element modeling techniques in dynamics as a design tool for landing and braking systems is discussed. Vibration mode shapes from the finite element analysis, including both whirl and squeal, are shown. Correlation between the finite element models and the experimental modal analyses of various system components are presented. Correlation between the performance of the complete landing and braking system model and the actual system during aircraft operation is also presented.