The First Law of Thermodynamics (FLT) applied to a closed non-stationary incompressible element of fluid is given as
$Q-W = \Delta(KE)+\Delta(PE)+\Delta U$ .......(Eq1)
where:
$\Delta U$ is change in internal energy;
$\Delta (KE)$ is the change in Kinetic energy;
$\Delta (PE)$ is the change in Potential energy;
$Q$ is the amount of heat supplied to the system;
$W$ is the amount of work done by the system to the environment.
(Let's assume $\Delta (PE)$ is zero)
If this element of fluid is going through a (converging)nozzle, from Bernoulli's law I can say that the pressure energy is transferred to kinetic energy, and at the end of the nozzle, the fluid's flow rate/velocity has increased. But how to deduce it from FLT applied to a closed non-stationary system (i.e $Eq1$) without using the Steady-flow-energy-equation(SFEE)/FLT-applied-to-open system?
The question is: I know how to analyze the flow through the nozzle as an Open system. How to do the same by applying FLW to a closed incompressible element of fluid passing the nozzle? How is the KE changing there are no pressure terms in Eq1 (and the is no PdV boundary work)?
PS: I am also trying to deduce how to apply the FLT to an incompressible element passing a turbine blade passage causing the turbine to rotate. Any help would be much appreciated.