Concept:
Hinlet = Hturbine + HL, stator + Guide + Hrotor + Hdraft tube + \(\frac{{V_3^2}}{{2g}}\) ... (i)
\({η _H} = \frac{{{H_{turbine}}}}{{{H_{inlet}}}}\)
Where, ηH is the hydraulic efficiency, HL, stator + Guide = Head loss in stator and guide vanes, V3 = Velocity at the exit of the draft tube, g = acceleration due to gravity
Calculation:
Given:
Hinlet = 200 m, HL, stator + Guide = 5 m, Hrotor = 10 m, Hdraft tube = 2 m, V3 = 3.5 m/s, g = 9.8 m/s2
From equation (i)
200 = Hturbine + 5 + 10 + 2 + \(\frac{{3.5^2}}{{2 \times 9.8}}\)
Hturbine = 182.375 m
∴ \({η _H} = \frac{{{H_{turbine}}}}{{{H_{inlet}}}}\) = \(\frac {182.375}{200}\) = 0.9118 = 91.87 %