xkybb
Civil/Environmental
- Sep 14, 2016
- 27
Hello!
According to my understanding, Stiffness Matrix Method is often applied for structural analysis (both computer and manual) in obtaining the forces/moments in structural elements.
However, it seems that the Stiffness Matrix Method and the Beam Curvature equation only works when the Material of the element is homogenous and isotopic, while in reality the structural elements are usually non homogenous (eg. a RC beam).
Therefore, let say in designing a RC frame, I wonder why it is OK to directly use the forces/moments obtained from stiffness matrix equation to design the structural elements without verifying the forces/moment by looping the analysis with the revised sectional properties with the provision of reinforcement?
Is that because the movement (eg.strain) of the section under loading will be smaller after the provision of reinforcement, and therefore the resultant forces/moment transfer to the structural elements must be smaller?
According to my understanding, Stiffness Matrix Method is often applied for structural analysis (both computer and manual) in obtaining the forces/moments in structural elements.
However, it seems that the Stiffness Matrix Method and the Beam Curvature equation only works when the Material of the element is homogenous and isotopic, while in reality the structural elements are usually non homogenous (eg. a RC beam).
Therefore, let say in designing a RC frame, I wonder why it is OK to directly use the forces/moments obtained from stiffness matrix equation to design the structural elements without verifying the forces/moment by looping the analysis with the revised sectional properties with the provision of reinforcement?
Is that because the movement (eg.strain) of the section under loading will be smaller after the provision of reinforcement, and therefore the resultant forces/moment transfer to the structural elements must be smaller?