Difference between Eulerian and Lagrangian formulation of Fluid Dynamics.
I am completely new to fluid mechanics. Until now definition $F = ma$ was sufficient for me to solve any rigid body problems in classical mechanics. With problems involving change of mass (for example, rocket propulsion) more basic definition comes to play, i.e. $F = \frac{\partial (mv)}{\partial t}$.
I tried to apply this definition to a fixed volume of sides $\Delta x, \Delta y, \Delta z$ respectively and proceeded as follows (in Eulerian frame): \begin{eqnarray} \mathbf{F} &=& \frac{\partial (m \mathbf{v})}{\partial t} \\ &=& \Delta x \Delta y \Delta z \frac{\partial (\rho \mathbf{v})}{\partial t} \\ &=& \Delta x \Delta y \Delta z \left[ \rho\frac{\partial ( \mathbf{v})}{\partial t} + \mathbf{v}\frac{\partial (\rho)}{\partial t} \right] \\ &=& \Delta x \Delta y \Delta z\left[ \rho\frac{\partial ( \mathbf{v})}{\partial t} - \mathbf{v}\left (\nabla (\rho \mathbf{v}) \right) \right] \qquad \text{ continuity equation} \\ \end{eqnarray}
The textbook proceeds as follows: Since $m\mathbf{v}$ is function of both velocity and space it is differentiated with respect to all variables to get total change, i.e.
\begin{eqnarray} \mathbf{F} &=& \frac{\partial (m \mathbf{v})}{\partial t} + \frac{\partial (m \mathbf{v})}{\partial x} \frac{\partial x}{\partial t} +\frac{\partial (m \mathbf{v})}{\partial y} \frac{\partial y}{\partial t} +\frac{\partial (m \mathbf{v})}{\partial z} \frac{\partial z}{\partial t}\\ &=& \Delta x \Delta y \Delta z \left[\frac{\partial (\rho \mathbf{v})}{\partial t} + \frac{\partial (\rho \mathbf{v})}{\partial x} v_x+\frac{\partial (\rho \mathbf{v})}{\partial y} v_y +\frac{\partial (\rho \mathbf{v})}{\partial z} v_z \right] \\ \end{eqnarray}
Clearly the two results are not identical. What am I missing here?