Introduction to Turbomachinery
1. Coordinate System
Total flow velocity is calculated based on below view as
The swirl (tangential) angle is (i)
Relative Velocities
Relative Velocity (ii)
Relative Flow Angle (iii)
Stream surface View Combining i, ii, and iii ;
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Introduction to Turbomachinery
2. Fundemental Laws used in Turbomachinery
2.1. Continuity Equation (Conservation of mass principle)
2.2. Conservation of Energy (1st law of thermodynamics)
Stagnation enthalpy;
if gz = 0;
For work producing machines
For work consuming machines
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Introduction to Turbomachinery
2. Fundemental Laws used in Turbomachinery
2.3. Conservation of Momentum (Newtons Second Law of Motion)
• For a steady flow process;
• Here, pA is the pressure contribution, where it is cancelled when there is rotational symmetry. Using
this basic rule one can determine the angular momentum as
• The Euler work equation is:
where
The Euler Pump equation
The Euler Turbine equation
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Introduction to Turbomachinery
2. Fundemental Laws used in Turbomachinery
Writing the Euler Eqution in the energy equation for
an adiabatic turbine or pump system (Q=0)
NOTE: Frictional losses are not included in the Euler Equation.
2.4. Rothalpy
An important property for fluid flow in rotating systems is called rothalpy (I)
and
Writing the velocity (c) , in terms of relative velocities :
, simplifying;
Defining a new RELATIVE stagnation enthalpy;
Redefining the Rothalpy:
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