The steady flow energy equation relates to open systems working under steady conditions i.e in which conditions do not change with
time.
The boundary encloses a system through which fluid flows at a constant rate, whilst heat transfer occurs
and external work is done all under steady conditions ,that is , the rates of mass flow
and energy flow are constant with respect to time.
The equation for steady flow ( the steady flow energy equation ) is generally written per unit mass as
q = heat transfer across boundary per unit mass
w = external work done by system per unit mass
z = fluid height
v = fluid velocity
h = fluid enthalpy ( u (internal energy + pv (pressure.specific volume)
Note in the examples below the system control volumes are defined by the red dashed line.
Potential energy (z) assumed to be constant..
Kinetic energy changes (1 to 2) assumed to be very small
Heater
w = 0 therefore
q = h2-h1
Potential energy (z) assumed to be constant..
Kinetic energy changes (1 to 2) assumed to be very small
Turbine
q = 0 therefore
w = h2-h1
Potential energy (z) assumed to be constant..
The higher velocity at orifice section is dissipated in tube downstream of the orifice and
therefore the kinetic energies at 1 and 2 are similar
Orifice
q = w = 0 therefore
therefore h1 = h2
Potential energy (z) assumed to be constant..
Kinetic energy changes are assumed to be significant
Nozzle
q = w = 0 therefore
(v22 - v12 ) /2 = (h1 - h2 )