A radial flow hydraulic turbine produces 32 kW under a head of 16mand running at 100 rpm. A geometrically similar model producing 42 kW and a head of 6mis to be tested under geometrically similar conditions. If model efficiency is assumed to be 92%, find the diameter ratio between the model and prototype, the volume flow rate through the model, and speed of the model.
Assuming constant fluid density, equating head, flow, and power coefficients, using subscripts 1 for the prototype and 2 for the model, we have from Eq. (1.19),
\frac{P_1} {(ρ_1N^3_1D^5_1)} = \frac{P_2} {(ρ_2N^3_2D^5_2)}, where ρ_1 = ρ_2.
Then,
\frac{D_2} {D_1} = \left(\frac{P_2} {P_1}\right)^{\frac{1}{5}}\left(\frac{N_1} {N_2}\right)^{\frac{3}{5}} \text{or} \frac{D_2}{D_1} = \left(\frac{0.032}{42}\right)^{\frac{1}{2}}\left(\frac{N_1} {N_2}\right)^{\frac{3}{5}} = 0.238\left(\frac{N_1} {N_2}\right)^{\frac{3}{5}}
Also, we know from Eq. (1.19) that
L_r = \frac{L_p } {L_m} = \frac{B_p}{B_m} = \frac{D_p} {D_m} (1.19)
\frac{gH_1}{(N_1D_1)^2} = \frac{gH_2}{(N_2D_2)^2}(gravity remains constant)
Then \frac{D_2} {D_1} = \left(\frac{H_2} {H_1}\right)^{\frac{1}{2}}\left(\frac{N_1} {N_2}\right) = \left(\frac{6}{16}\right)^{\frac{1}{2}} \left(\frac{N_1}{N_2}\right)
Equating the diameter ratios, we get
0.238 \left(\frac{N_1} {N_2}\right)^{\frac{3}{5}} = \left(\frac{6}{16}\right)^{\frac{1}{2}} \left(\frac{N_1}{N_2}\right)
or
\left(\frac{N_1} {N_2}\right)^{\frac{3}{5}} = \frac{0.612}{0.238} = 2.57
Therefore the model speed is
N_2 = 100 × (2.57)^{\frac{5}{2}} = 1059 rpm
Model scale ratio is given by
\frac{D_2} {D_1} = (0.238) \left(\frac{100} {1059}\right)^{\frac{3}{5}} = 0.238(0.094)^{0.6} = 0.058.
Model efficiency is η_m = \frac{\text{Power output}} {\text{Water power input}}
or,
0.92 = \frac{42 × 10^3} {ρgQH},
or,
Q = \frac{42 × 10^3}{0.92 × 10^3 × 9.81 × 6} = 0.776 m³/s