Wantstolearn
Mechanical
- Jul 7, 2000
- 6
The problem that I am having is being able to justify that the member that I am analyzing is connected to a rigid body. I am in the process of design highway vessels and they require rollover protection. My analysis is based on the assumption that the tank with stiffener rings are considered rigid in order for me to validate the design of the rollover protection.
I have considered a case where the rollover protection is connected directly to the shell (with a repad) and that only that plate material will resist the forces and moments translated through from the forces applied to the upper part of the rollover protection. Calculating the moment of inertia for the shell and the pad I get a certain value. Then I have considered a case where the rollover protection is mounted around the stiffener rings (flat bar rolled on edge and welded to the tank). Recaculating the moment of intertia, we find that with similar sized repads, and only the addition of the stiffener ring, that same section of shell is now has a moment of inertia that is 16X greater than the previous case (both M.O.I's considered about the N.A. of the geometry) Does this constitute rigid if the shells are to be considered non rigid?
Also, How would this apply if the stiffener ring is close by where "edge effects" with the proximity of the stiffener ring may play a role. If it does play a role, How far away until these effects can be neglected.
Obviously in the real world there is no such thing as a perfectly stiff/rigid structure, but I need to learn how I can determine " the degree of stiffeness" in order for me to understand the risks in making a rigid base assumption.
Thanks
I have considered a case where the rollover protection is connected directly to the shell (with a repad) and that only that plate material will resist the forces and moments translated through from the forces applied to the upper part of the rollover protection. Calculating the moment of inertia for the shell and the pad I get a certain value. Then I have considered a case where the rollover protection is mounted around the stiffener rings (flat bar rolled on edge and welded to the tank). Recaculating the moment of intertia, we find that with similar sized repads, and only the addition of the stiffener ring, that same section of shell is now has a moment of inertia that is 16X greater than the previous case (both M.O.I's considered about the N.A. of the geometry) Does this constitute rigid if the shells are to be considered non rigid?
Also, How would this apply if the stiffener ring is close by where "edge effects" with the proximity of the stiffener ring may play a role. If it does play a role, How far away until these effects can be neglected.
Obviously in the real world there is no such thing as a perfectly stiff/rigid structure, but I need to learn how I can determine " the degree of stiffeness" in order for me to understand the risks in making a rigid base assumption.
Thanks