Turbomachinery – Euler’s Equation ME 362 Page 1 of 4 Centrifugal Pump: W2 V2 V2 2 2 Flow Direction U2 Subscript: W1 1 V1 1 1 - inlet 2 - exit V1 U1 Velocity Triangle: V W W Vr V U circumferential speed of impeller ( U r ) velocity tangent to blade surface absolute velocity ( V U W ) radial component of V circumferential component of V blade angle U: W: V: Vr: V: : To construct a velocity triangle: Draw U tangent to the rotor Draw W tangent to the blade surface Draw V radial circumferential Turbomachinery – Euler’s Equation ME 362 Page 2 of 4 Euler Turbomachine Equation: Shaft torque: Tshaft Qr2V 2 r1V 1 Brake horsepower: bhp QU 2V 2 U 1V 1 Note: Euler’s equation is valid for both pump and turbine bhp is the power required to drive shaft of pump (bhp > 0) or the power required to deliver to shaft of turbine (bhp < 0) Pump vs. Turbine: 2 Pump 1 U2 (exit) > U1 (inlet) V2 (exit) > V1 (inlet) bhp > 0 U2 (exit) < U1 (inlet) V2 (exit) < V1 (inlet) bhp < 0 1 Turbine 2 Pump Performance Characteristics: Water horsepower: Pw gQH Pump efficiency: Pw (1) bhp where Pw: H = hs - hL: hs: hL: power delivered to fluid available head shaft work head head loss Turbomachinery – Euler’s Equation ME 362 Pump in Ideal Flow Condition: Ideal flow condition: = 1 (no head loss) and V1 = 0 (maximum bhp) Velocity triangle at the inlet: W1 radial 1 V1 U1 circumferential U1 r1 Vr1 V1 U1 tan 1 Q1 2r1bVr1 (b = blade height) Velocity triangle at the exit: W2 V2 Vr2 V2 radial 2 U2 circumferential Vr2cot2 U 2 r2 Q2 2r2bVr 2 Q1 Vr 2 Q2 2r2 b V 2 U 2 Vr 2 cot 2 U 2V 2 g Ideal head: Hi Maximum power: bhp Pw gQH i QU 2V 2 ( = 1) Page 3 of 4 Turbomachinery – Euler’s Equation ME 362 Page 4 of 4 Examples: Problem 1 (Pump): Given pump geometry and specifications on the figure below. Assume ideal flow condition. Find the power required to drive it. 0.75” 55 = 1.94 slugs/ft3 Q = 0.25 ft3/s = 960 rpm V1 4” 12” 960 rpm 0.25 ft3/s Problem 2 (Turbine): A water turbine with radial flow has the dimensions shown below. The absolute entering velocity is 50 ft/s, and it makes an angle of 30 with the tangent to the rotor. The absolute exit velocity is directed radially inward. The angular speed of the rotor is 120 rpm. Find the power delivered to the shaft of the turbine. V1 30 b r1 V2 r2 V1 = 50 ft/s = 120 rpm r1 = 2 ft r2 = 1 ft b = 1 ft = 1.94 slug/ft3