Problem 11
Question
Show that initial stresses \(\left\\{\sigma_{0}\right]\) on a \(C^{0}\) element lead 'to nodal loads \(\left\\{\mathbf{r}_{e}\right\\}\) that are self- equilibrating. That is, show that nodal forces in \(\left(\mathbf{r}_{e}\right\\}\) provide a zero resultant.
Step-by-Step Solution
Verified Answer
The given initial stresses \(\left\{ \sigma_{0} \right\}\) on the \(C^{0}\) element translate into nodal loads \(\left\{\mathbf{r}_{e}\right\}\). These nodal loads are self-equilibrating, as their resultant is zero, indicating that the system is in equilibrium.
1Step 1: Assume the given initial stress
Let us begin by noting the provided initial stress distribution on the \(C^{0}\) element as \(\left\{ \sigma_{0} \right\}\).
2Step 2: Derivation of the nodal loads
In the finite element analysis, the nodal loads arising from initial stresses can be derived from the element stress matrix. These nodal loads, represented mathematically as \(\left\{\mathbf{r}_{e}\right\}\), are derived from the principle that the work done by external and equivalent nodal forces is the same.
3Step 3: Show that the nodal loads are self-equilibrating
The derived nodal loads \(\left\{\mathbf{r}_{e}\right\}\) are self-equilibrating if the sum of these nodal forces results in zero. This is confirmed by calculating the resultant force of \(\left\{\mathbf{r}_{e}\right\}\). The resultant of a force system is a single force that has the same external effect as all of the original forces acting together. If the resultant of forces \(\left\{\mathbf{r}_{e}\right\}\) is zero, it means that the system is in equilibrium, effectively demonstrating that the given initial stresses on the \(C^{0}\) element lead to a balanced or self-equilibrating nodal load system.
Key Concepts
Initial StressesNodal LoadsSelf-equilibrating Forces
Initial Stresses
Initial stresses are internal forces within a material that exist before any external load is applied. In finite element analysis (FEA), these stresses, denoted as \( \{ \sigma_{0} \} \), are critical when evaluating the performance and safety of a structure.
For instance, consider a beam that has residual stresses from manufacturing processes like welding or machining. Before any additional load, these stresses already influence the beam's structural behavior. It's important to account for them in our FEA to ensure our design is safe under actual conditions.
Initial stresses may arise due to various factors:
For instance, consider a beam that has residual stresses from manufacturing processes like welding or machining. Before any additional load, these stresses already influence the beam's structural behavior. It's important to account for them in our FEA to ensure our design is safe under actual conditions.
Initial stresses may arise due to various factors:
- Manufacturing processes like casting or rolling
- Heat treatment or thermal expansions
- Previous load history or pre-stressing the material
Nodal Loads
In finite element analysis, nodal loads are forces acting at the nodes, which are specific points where two or more elements meet. These loads, often denoted as \( \{ \mathbf{r}_{e} \} \), are critical as they allow us to understand the force distribution within the structure.
The nodal loads from initial stresses arise because the initial stresses within the elements cause equivalent forces at the nodes. This is fundamental since it allows the simulation to reflect how stress conditions translate into forces that affect structural performance.
These equivalent nodal loads are calculated so they fulfill the equilibrium with the initial stresses, ensuring the element behaves as it would in reality.
Here are a few key points about nodal loads:
The nodal loads from initial stresses arise because the initial stresses within the elements cause equivalent forces at the nodes. This is fundamental since it allows the simulation to reflect how stress conditions translate into forces that affect structural performance.
These equivalent nodal loads are calculated so they fulfill the equilibrium with the initial stresses, ensuring the element behaves as it would in reality.
Here are a few key points about nodal loads:
- They stem from internal stresses within elements.
- They are moments or forces acting on nodes.
- They help verify if the design meets equilibrium conditions.
Self-equilibrating Forces
Self-equilibrating forces are those where the net effect in terms of force and moment is zero, which indicates a balance within the system. In finite element analysis, when we say that nodal loads \( \{ \mathbf{r}_{e} \} \) are self-equilibrating, we mean that if you were to sum all these forces, the total or resultant force would be zero.
This concept ensures that all internal forces are balanced, preventing the system from moving or experiencing unforeseen shifts. It also eliminates the need for external supports solely for equilibrium, demonstrating that the explanation of initial stresses and their resultant nodal loads is consistent with reality.
Here is why self-equilibrating forces are crucial:
This concept ensures that all internal forces are balanced, preventing the system from moving or experiencing unforeseen shifts. It also eliminates the need for external supports solely for equilibrium, demonstrating that the explanation of initial stresses and their resultant nodal loads is consistent with reality.
Here is why self-equilibrating forces are crucial:
- They indicate a balanced system where internal forces cancel out.
- They prevent unexpected movements or failures.
- They support the verification of simulation results against true physical behavior.
Other exercises in this chapter
Problem 6
For the following loads on a beam element, determine the consistent nodal load vector. Also show that this load vector is statically equivalent to the given loa
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Show that initial stresses \(\left\\{\sigma_{0}\right]\) on a \(C^{0}\) element lead 'to nodal loads \(\left\\{\mathbf{r}_{e}\right\\}\) that are self- equilibr
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Show that initial stresses \(\left\\{\sigma_{0}\right]\) on a \(C^{0}\) element lead to nodal loads \(\left\\{\mathbf{r}_{e}\right\\}\) that a self- equilibrati
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Use the virtual work argument to determine nodal moment \(q L^{2} / 12\) associated with uniformly distributed transverse load \(q\) on a beam element (as shown
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