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Question:
give answer in 2 step with explanation at the end of each step and final answer at the end:
CC mmr———]
Fem
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ws
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ES)
=
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Asked by: Rahul
Created at: 2025-12-14 03:06:41
Asked by: Rahul
Created at: 2025-12-14 03:06:41
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# Solution to Finite Volume Problem (Step-by-Step)
Let's break down the solution into two main steps as requested, with explanations at the end of each step.
---
## **Step 1: Discretization Using the Finite Volume Method**
### **Given Data**
- Plate separation, \( H = .005 \) m
- Number of cells, \( N = 3 \) (from the diagram)
- Each cell width, \( \Delta y = H/N = .005/3 = .00167 \) m
- Fluid viscosity, \( \mu = .001 \) Pa·s
- Pressure gradient, \( \frac{dp}{dx} = -12 \) Pa/m
- Lower plate velocity, \( u_ = \)
- Upper plate velocity, \( u_s = .5 \) m/s
### **Governing Equation**
The x-momentum equation simplifies to:
\[
\frac{d^2u}{dy^2} = \frac{1}{\mu} \frac{dp}{dx}
\]
### **Finite Volume Discretization**
For each cell centered at \( y_1 \), \( y_2 \), \( y_3 \):
- The finite volume approach uses the midpoint for velocities (\( u_1, u_2, u_3 \)).
- At each cell, the discretized form (central difference) is:
\[
\frac{u_{i+1} - 2u_i + u_{i-1}}{\Delta y^2} = \frac{1}{\mu}\frac{dp}{dx}
\]
where \( i = 1, 2, 3 \).
#### **Boundary Conditions**
- \( u_ = \) (stationary lower plate)
- \( u_4 = u_s = .5 \) m/s (moving upper plate)
#### **Write the Equations**
- For cell 1: \( \frac{u_2 - 2u_1 + u_}{\Delta y^2} = S \)
- For cell 2: \( \frac{u_3 - 2u_2 + u_1}{\Delta y^2} = S \)
- For cell 3: \( \frac{u_4 - 2u_3 + u_2}{\Delta y^2} = S \)
Where \( S = \frac{1}{\mu}\frac{dp}{dx} = \frac{-12}{.001} = -12000 \) 1/s².
**Explanation:**
Here, we have discretized the x-momentum equation using the finite volume method and set up a system of equations for the unknown velocities at the cell centers, incorporating the boundary conditions.
---
## **Step 2: Construct and Solve the Linear System**
### **Plug in Values**
- \( \Delta y^2 = (.00167)^2 = 2.78 \times 10^{-6} \)
- \( S = -12000 \)
Now substitute into each equation:
**Cell 1:**
\[
\frac{u_2 - 2u_1 + u_}{2.78 \times 10^{-6}} = -12000
\]
\[
u_2 - 2u_1 + = -12000 \times 2.78 \times 10^{-6}
\]
\[
u_2 - 2u_1 = -.0334
\]
**Cell 2:**
\[
\frac{u_3 - 2u_2 + u_1}{2.78 \times 10^{-6}} = -12000
\]
\[
u_3 - 2u_2 + u_1 = -.0334
\]
**Cell 3:**
\[
\frac{u_4 - 2u_3 + u_2}{2.78 \times 10^{-6}} = -12000
\]
\[
.5 - 2u_3 + u_2 = -.0334
\]
\[
-2u_3 + u_2 = -.5334
\]
### **Solve the System**
Now, solve for \( u_1, u_2, u_3 \):
1. \( u_2 - 2u_1 = -.0334 \)
2. \( u_3 - 2u_2 + u_1 = -.0334 \)
3. \( -2u_3 + u_2 = -.5334 \)
Let's write these as simultaneous equations:
1. \( -2u_1 + u_2 = -.0334 \)
2. \( u_1 - 2u_2 + u_3 = -.0334 \)
3. \( u_2 - 2u_3 = -.5334 \)
Now solve step-by-step:
- From (3): \( u_2 = -.5334 + 2u_3 \)
- Substitute into (2):
\( u_1 - 2(-.5334 + 2u_3) + u_3 = -.0334 \)
\( u_1 + 1.0668 - 4u_3 + u_3 = -.0334 \)
\( u_1 - 3u_3 = -1.1002 \) (A)
- From (1):
\( -2u_1 + (-.5334 + 2u_3) = -.0334 \)
\( -2u_1 - .5334 + 2u_3 = -.0334 \)
\( -2u_1 + 2u_3 = .5 \)
\( -2u_1 + 2u_3 = .5 \)
\( -u_1 + u_3 = .25 \)
\( u_1 = u_3 - .25 \) (B)
Now substitute (B) in (A):
\( (u_3 - .25) - 3u_3 = -1.1002 \)
\( u_3 - .25 - 3u_3 = -1.1002 \)
\( -2u_3 - .25 = -1.1002 \)
\( -2u_3 = -.8502 \)
\( u_3 = .4251 \) m/s
Now, \( u_1 = u_3 - .25 = .4251 - .25 = .1751 \) m/s
Now, \( u_2 = -.5334 + 2u_3 = -.5334 + 2 \times .4251 = -.5334 + .8502 = .3168 \) m/s
---
**Explanation:**
We substituted the known boundary values and solved the resulting system of equations step by step to obtain the velocities at each cell center.
---
## **Final Answers**
- **Cell 1 center velocity (\( u_1 \)):** **.175 m/s**
- **Cell 2 center velocity (\( u_2 \)):** **.317 m/s**
- **Cell 3 center velocity (\( u_3 \)):** **.425 m/s**
- **Upper plate velocity (\( u_s \)):** **.5 m/s** (given)
---
### **Summary Table**
| Location | Velocity (m/s) |
|------------------|:-------------:|
| \( u_ \) (bottom plate) | |
| \( u_1 \) (cell 1 center) | .175 |
| \( u_2 \) (cell 2 center) | .317 |
| \( u_3 \) (cell 3 center) | .425 |
| \( u_4 \) (top plate) | .5 |
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