- #1
Saladsamurai
- 3,020
- 7
Homework Statement
I need to derive the 2D N-S equations for steady, incompressible, constant viscosity flow in the xy-plane. I need to use a control volume approach (as opposed to system approach) on a differential control volume (CV) using the conseervation of linear momentum.
Homework Equations
Conservation of Linear Momentum for a CV is given by:
[tex]\mathbf{F} = \frac{\partial{}}{\partial{t}}\int_v\mathbf{V}\rho\,dv + \int_{A_{in}}\mathbf{V}\rho(\mathbf{V}\cdot\hat{n})\,dA_{in}
+ \int_{A_{out}}\mathbf{V}\rho(\mathbf{V}\cdot\hat{n})\,dA_{out}
\qquad(1)[/tex]
The Attempt at a Solution
My problem is with the application of (1). I have a control volume with dimensions dx,dy,1 (unit depth). Now (1) is a vector equation so it can (and probably should) be divided up into its components. We know it is steady and hence the first term in (1) goes to zero.
Note that [itex]\mathbf{V} = u\hat{i} + v\hat{j}[/itex]
x-momentum:
[tex]
F_x = \int u\rho \left [u\hat{i}\cdot(-\hat{i})\right ]\,dy(1)
+
\int (u+\frac{\partial{u}}{\partial{x}}\,dx)\rho(u+\frac{\partial{u}}{\partial{x}}\,dx)\hat{i}\cdot\hat{i}\,dy(1)
[/tex]
Now I know that I can simplify some things here, but
i) Does this look correct?
ii) What are the bounds of my integrals?
Any advice is appreciated.