Table of contents | |
Newton’s Law of Viscosity | |
Variation of Viscosity with Temperature | |
Types of Fluids | |
Rheological Classification of Fluids | |
Thermodynamic Properties | |
Solved Numericals |
Fluids which obey the above relation are known as Newtonain fluids and the fluids which do not obey the above relation are called Non−Newtonain fluids.
The relation between viscosity and temperature for liquids and gases is :
For Liquids,
where μ = Viscosity of liquid at t°C, in poise
μ0 = Viscosity of liquid at 0°C, in poise
α, β are constants for the liquid
For water, μ0 = 1.79 × 10−3 poise, α = 0.03368 and β = 0.000221
For gases, μ = μ0 + αt − βt2
where for air; μ0 = 0.000017, α = 0.000000056, β = 0.1189 × 10−9
Ideal Fluid: An ideal fluid is an imaginary fluid that is incompressible (density remains constant) and has no viscosity (internal friction). It serves as a theoretical model and does not exist in reality.
Real Fluid: A real fluid is any fluid that possesses viscosity, which is the resistance to flow. In practical terms, all fluids encountered in everyday life, such as water, oil, and air, are real fluids.
Newtonian Fluid: A Newtonian fluid is a type of real fluid that obeys Newton's law of viscosity. According to this law, the shear stress between adjacent fluid layers is directly proportional to the velocity gradient (rate of change of velocity with respect to distance) in the direction perpendicular to the layers.
Non-Newtonian Fluid: A non-Newtonian fluid is a real fluid that does not obey Newton's law of viscosity under all conditions. These fluids may exhibit shear-thinning (viscosity decreases with increasing shear rate), shear-thickening (viscosity increases with increasing shear rate), or other types of complex behaviors depending on the applied stress or shear rate.
Ideal Plastic Fluid: An ideal plastic fluid is a type of non-Newtonian fluid where the shear stress is greater than a certain yield value (yield stress), and the shear stress is directly proportional to the rate of shear strain (velocity gradient) once the yield stress is exceeded. This means that the fluid behaves like a solid below the yield stress and flows like a fluid above it.
Above four cases are time independent. There are two time dependent purely viscous fluids governed by the following equations:
(i) Rheopectic fluids : f(t) increases with time.
(ii) Thixotropic fluids : f(t) decreases with time.
1. Isothermal Process : If the change in density occurs at constant temperature, then the process is called isothermal and relationship between pressure and density is given by
2. Adiabatic P rocess : If the change in density occurs with no heat exchange to and from the gas, the process is called adiabatic. And if no heat generated within the gas due to friction, the relationship between pressure and density is given by
where k = Ratio of specific heat of a gas at constant pressure and constant volume = 1.4 for air
Another form of equation of state ; PV = nRT
where V = volume of gas
n = number of moles in a volume of gas
R = universal gas constant = 8.314 × 103 J/kg−mole K.
Q1: The 'momentum correction factor' for a laminar flow through a circular pipe is:
Ans: Momentum correction factor - The momentum correction factor is defined as the ratio of momentum of the flow per second based on actual velocity to the momentum of the flow per second based on average velocity across a section.For laminar flow through a circular pipe, β = 4/3 = 1.33
Q2: The velocity distribution over one half of a cross section is uniform and is zero over the remaining half. The momentum correction factor for this cross section is
Ans: The momentum correction factor is defined as the ratio of momentum of the flow per second based on actual velocity to the momentum of the flow per second based on average velocity across a section.
u = actual velocity, V = average velocity
Calculation:
Q3: The velocity distribution over one half of a cross section is uniform and is zero over the remaining half. The momentum correction factor for this cross section is
Ans: The momentum correction factor is defined as the ratio of momentum of the flow per second based on actual velocity to the momentum of the flow per second based on average velocity across a section.
u = actual velocity, V = average velocity
Calculation:
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