The wing is considered as euler-bernoulli beam which is attached to the main fuselage and this fuselage is considered having translational motion. Both the engines are considered as lumped masses so basically a euler bernoulli beam having two lumped masses fixed from one end to the fuselage...
Hi there,
I am currently a student at Heriot-Watt University and have been given a project of deriving a nonlinear equation of motion for an a380 wing engine. The engine is to be considered as a lumped mass attached to the cantilever beam and the main fuselage is considered having translational...