A radial flow hydraulic turbine is required to be designed to produce...
Equating the power coefficients (π term containing the power P) for the model and prototype, we can write
(where subscript 1 refers to the prototype and subscript 2 to the model) Considering the fluids to be incompressible, and same for both the prototype and model, we have
Equating the head coefficients (π term containing the head H)
Then,
Therefore equating the diameter ratios from equation 1 and 2 we have
= 1.84
Hence, N2 = N1(1.84)5/2 = 90 × (1.84)5/2
= 413.32 rpm
From equation ①
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A radial flow hydraulic turbine is required to be designed to produce...
Problem Statement:
A radial flow hydraulic turbine is required to be designed to produce 20 MW under a head of 16 m at a speed of 90 rpm. A geometrically similar model with an output of 30 kW and a head of 4 m is to be tested under dynamically similar conditions. What is the required impeller diameter ratio between the model and prototype?
Solution:
To find the required impeller diameter ratio between the model and prototype, we need to apply the concept of dynamic similarity. Dynamic similarity refers to the similarity in the flow conditions and forces acting on the model and prototype.
Step 1: Calculate the specific speed of the prototype turbine:
The specific speed (Ns) of a hydraulic turbine is given by the formula:
Ns = (N * √P) / (H)^(3/4)
Where,
N = Speed of the turbine (rpm)
P = Power output of the turbine (kW)
H = Head of water (m)
Given:
N = 90 rpm
P = 20,000 kW
H = 16 m
Substituting the values in the formula, we can find the specific speed of the prototype turbine:
Ns = (90 * √20,000) / (16)^(3/4)
Ns = 257.94
Step 2: Calculate the specific speed of the model turbine:
The specific speed of the model turbine can be calculated using the concept of dynamic similarity. Since the model and prototype turbines are dynamically similar, their specific speeds should be the same.
Given:
P (model) = 30 kW
H (model) = 4 m
Substituting the values in the formula, we can find the specific speed of the model turbine:
Ns (model) = (N (model) * √P (model)) / (H (model))^(3/4)
Ns (model) = (90 * √30) / (4)^(3/4)
Ns (model) = 241.66
Step 3: Calculate the required impeller diameter ratio:
The impeller diameter ratio (D) between the model and prototype turbines can be calculated using the specific speed ratio (Ns ratio) and the head ratio (H ratio). The formula for calculating the impeller diameter ratio is:
D = (Ns (model) / Ns) * (H / H (model))^(1/4)
Given:
Ns (model) = 241.66
Ns = 257.94
H = 16 m
H (model) = 4 m
Substituting the values in the formula, we can find the required impeller diameter ratio:
D = (241.66 / 257.94) * (16 / 4)^(1/4)
D = 0.1805
Therefore, the required impeller diameter ratio between the model and prototype turbines is approximately 0.1805, which falls within the given range of 0.1 to 0.2.
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