Water of kinematic viscosity v = 1 centistoke flows through a 10 mm di...
Water of kinematic viscosity v = 1 centistoke flows through a 10 mm di...
Kinematic viscosity:
- Kinematic viscosity (ν) is a measure of the internal friction or resistance to flow within a fluid.
- It is defined as the ratio of dynamic viscosity (μ) to the density of the fluid (ρ).
- Mathematically, ν = μ/ρ.
- The SI unit of kinematic viscosity is square meter per second (m²/s), but it is often expressed in centistokes (cSt) in engineering applications.
Critical flow:
- Critical flow refers to the condition where the flow velocity reaches the sonic velocity (also known as the speed of sound) at some point within a fluid system.
- In this case, the flow velocity at the throat of the pipe reaches the sonic velocity.
- At critical flow, the flow rate cannot be increased any further by increasing the pressure difference across the pipe.
- Critical flow is also associated with the maximum possible discharge through a given pipe diameter.
Calculation:
Given:
- Kinematic viscosity (ν) = 1 centistoke = 0.0001 m²/s
- Pipe diameter = 10 mm = 0.01 m
To find the critical flow, we can use the concept of the Reynolds number (Re) and Mach number (Ma).
Reynolds number:
- The Reynolds number is a dimensionless quantity that characterizes the flow regime of a fluid.
- It is defined as the ratio of the inertial forces to the viscous forces within the fluid.
- Mathematically, Re = (ρVD)/μ, where V is the velocity of the flow, D is the characteristic length (pipe diameter), ρ is the density, and μ is the dynamic viscosity.
- At critical flow, the Reynolds number is typically around 2,000.
Mach number:
- The Mach number is a dimensionless quantity that represents the ratio of the flow velocity to the speed of sound.
- Mathematically, Ma = V/a, where V is the flow velocity and a is the speed of sound.
- At critical flow, the Mach number is equal to 1.
To determine the critical flow, we need to find the flow velocity (V) at the throat of the pipe.
Using Reynolds number:
- Rearranging the Reynolds number equation, we have V = (Reμ)/(ρD).
- Substituting the given values, we get V = (2000 * 0.0001)/(ρ * 0.01).
- Since the density of water is approximately 1000 kg/m³, V = 0.2 m/s.
Using Mach number:
- At critical flow, the Mach number is 1. Therefore, V = a.
- The speed of sound in water at room temperature is approximately 1482 m/s.
Therefore, the flow velocity at the throat of the pipe is 0.2 m/s, and the critical flow corresponds to a discharge of approximately 0.016 L/s (0.02 L/s when rounded to two decimal places). Hence, the correct answer is option 'C' (0.016 L/s).
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