generaluday
Automotive
- May 5, 2011
- 14
Hello!
I'm trying to solve a problem comprising of a simple fuselage with pre-stressed tension cables connecting the arms of the fuselage. I'd like to conduct a modal analysis on this setup. Let's assume that the fuselage comprises of an X-shaped structure with 4 tension cables connecting the arms, and is tethered to the ground along it's center point. I've meshed the arms with simple Beam elements, and I tried using DOF Spring elements with a certain stiffness for the cables, but the modal frequencies seem to remain the same regardless of the changes in the stiffness values.
It has been well established that the tension in the cables is critical in determining the natural frequencies of such structures, for instance, those of cable-stayed bridges, etc. What is the best way to simulate this type of scenario in Femap?
Thanks.
I'm trying to solve a problem comprising of a simple fuselage with pre-stressed tension cables connecting the arms of the fuselage. I'd like to conduct a modal analysis on this setup. Let's assume that the fuselage comprises of an X-shaped structure with 4 tension cables connecting the arms, and is tethered to the ground along it's center point. I've meshed the arms with simple Beam elements, and I tried using DOF Spring elements with a certain stiffness for the cables, but the modal frequencies seem to remain the same regardless of the changes in the stiffness values.
It has been well established that the tension in the cables is critical in determining the natural frequencies of such structures, for instance, those of cable-stayed bridges, etc. What is the best way to simulate this type of scenario in Femap?
Thanks.