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Euler's pump and turbine equation
Turbomachinery Equation in Fluid Dynamics
Turbomachinery Equation in Fluid Dynamics
The Euler pump and turbine equations are the most fundamental equations in the field of turbomachinery. These equations govern the power, efficiencies and other factors that contribute to the design of turbomachines. With the help of these equations the head developed by a pump and the head utilised by a turbine can be easily determined. As the name suggests these equations were formulated by Leonhard Euler in the eighteenth century.See:
- Euler (1752) "Maximes pour arranger le plus avantageusement les machines destinées à élever de l'eau par moyen des pompes" (Maxims for arranging most advantageously machines intended to raise water by means of pumps), Mémoires de l'Académie Royale des Sciences et des Belles Lettres à Berlin, 8 : 185-232. Here, Euler presents his results for maximizing the outputs of windmills and water wheels, among other means of powering pumps.
- Euler (1754) "Théorie plus complette des machines qui sont mises en mouvement par la réaction de l'eau" (More complete theory of machines that are set in motion by reaction with water), Mémoires de l'Académie Royale des Sciences et des Belles Lettres à Berlin, 10 : 227-295. An analysis of Segner's wheel.
- Euler (1756) "Recherches plus exactes sur l'effect des moulins à vent" (More exact research on the effect [i.e., work output] of windmills), Mémoires de l'Académie Royale des Sciences et des Belles Lettres à Berlin, 12 : 166-234. These equations can be derived from the moment of momentum equation when applied for a pump or a turbine.
Conservation of angular momentum
A consequence of Newton's second law of mechanics is the conservation of the angular momentum (or the “moment of momentum”) which is fundamental to all turbomachines. Accordingly, the change of the angular momentum is equal to the sum of the external moments. The variation of angular momentum \rho\cdot Q\cdot r\cdot c_u at inlet and outlet, an external torque M and friction moments due to shear stresses M_\tau act on an impeller or a diffuser.
Since no pressure forces are created on cylindrical surfaces in the circumferential direction, it is possible to write:
:\rho Q (c_{2u} r_2 - c_{1u} r_1) = M + M_{\tau}, (1.13){{cite book
:c_{2u}=c_2\cos\alpha_2, :c_{1u}=c_1\cos\alpha_1.,
Velocity triangles
The color triangles formed by velocity vectors u,c and w are called velocity triangles and are helpful in explaining how pumps work.
:c_1, and c_2, are the absolute velocities of the fluid at the inlet and outlet respectively.
:w_1, and w_2, are the relative velocities of the fluid with respect to the blade at the inlet and outlet respectively.
:u_1, and u_2, are the velocities of the blade at the inlet and outlet respectively.
:\omega is angular velocity.
Figures 'a' and 'b' show impellers with backward and forward-curved vanes respectively.
Euler's pump equation
Based on Eq.(1.13), Euler developed the equation for the pressure head created by an impeller:
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