kotawsu
Mechanical
- Dec 26, 2004
- 76
Hello everybody. I have been simulating a bolted joint connection in abaqus. I am trying to understand the load distribution between the joint and the bolt when an external compressive load is applied. I know that there is a formula
Fb= Fp-N*F
where Fb---bolt load
N--load factor
F--external applied load
I understand that when an external load(compressive on the members) is applied the bolt load relaxes than th pretension load and the joint load increases. But when my analysis results is showing me a decrease in both bolt load and the joint load. The shape of the joint is not flat-flat panel. The upper panel is a z-shape beam and the lower panel is a flat panle. I was wondering if this could happen or is there any otehr formula by wich i can calculate that factor(the portion of the external load which relaxes the bolt load). Thanks for your time and patience.
Kota
Fb= Fp-N*F
where Fb---bolt load
N--load factor
F--external applied load
I understand that when an external load(compressive on the members) is applied the bolt load relaxes than th pretension load and the joint load increases. But when my analysis results is showing me a decrease in both bolt load and the joint load. The shape of the joint is not flat-flat panel. The upper panel is a z-shape beam and the lower panel is a flat panle. I was wondering if this could happen or is there any otehr formula by wich i can calculate that factor(the portion of the external load which relaxes the bolt load). Thanks for your time and patience.
Kota