amorrison
Mechanical
- Dec 21, 2000
- 605
Say you have a basic concept aircraft structural design.
In flying mode various loads will be put on the structure - by the flaps, elevator, rudder etc. which in the real world is taken up by rotational mass inertia of the aircraft structual materials.
FE support reaction member problem.
In an simple FE simulation hard reaction points are used to balance these loads - but this produces high reaction values at these local reaction points and "distorts" the local reaction member stresses.
Any solutions.
Thanks.
In flying mode various loads will be put on the structure - by the flaps, elevator, rudder etc. which in the real world is taken up by rotational mass inertia of the aircraft structual materials.
FE support reaction member problem.
In an simple FE simulation hard reaction points are used to balance these loads - but this produces high reaction values at these local reaction points and "distorts" the local reaction member stresses.
Any solutions.
Thanks.