MECHANICAL PROPERTIES OF FLUIDS Mohamed Sherif K, HSST Physics, GHSS Athavanad.
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Transcript of MECHANICAL PROPERTIES OF FLUIDS Mohamed Sherif K, HSST Physics, GHSS Athavanad.
MECHANICAL PROPERTIES OF FLUIDS
Mohamed Sherif K, HSST Physics, GHSS Athavanad
FLUIDS
Fluid is a substance which can flow (air & liquid)Unlike a solid, a fluid has no definite shape of its own. Solids and liquids have a fixed volume, whereas a gas fills the entire volume of its container. Solids and liquids have lower compressibility compared to gases
10.2 PRESSURE
Average pressure (Pav) is normal force (F) acting per unit area (A).
Units : N/m2, Pascal , Atm (atmospheric pressure),Psi ,bar, torr1 atm =1.013×105 PascalPressure is a scalar quantity
Density (ρ)
Density is defined as mass per unit volume.
𝜌 = , V = 𝑀𝑎𝑠𝑠 𝑉𝑜𝑙𝑢𝑚𝑒Its unit is kg/m3.
Density of water at 40C is 103kg/m3. The relative density of a substance is the ratio of its density to the density of water at 4°C.
10.2.1 Pascal’s Law
Pressure inside a fluid at rest is same at all points if they are at the same height
10.2.2 Variation of Pressure with Depth
Consider,Pressure at point 1 = P1
Pressure at point 2 = P2
Mass of fluid inside cylinder = mArea of the base of cylinder = AHeight of the cylinder = hDensity of fluid =ρ
m = ρhA∴P2 − P1 = ρghWhen point 1 is open to atmosphere,P1 = Atmospheric pressure (Pa)P2 = P (absolute pressure)
∴ P = Pa + ρghGauge pressure = P − Pa = ρgh
Hydrostatic paradox
10.2.3 Atmospheric Pressure and Gauge Pressure
The pressure of the atmosphere at any point is equal to the weight of a column of air of unit cross sectional area extending from that point to the top of the atmosphere. At sea level it is 1.013 × 105 Pa (1 atm)
Pa = ρgh
76 cm at sea level equivalent to one atmosphere (1 atm)
A pressure equivalent of 1 mm is called a torr (after Torricelli).1 torr = 133 Pa.
In meteorology, a common unit is the bar and millibar.1 bar = 105 Pa
10.2.3 Atmospheric Pressure and Gauge Pressure
10.2.4 Hydraulic Machines
Pascal’s law for transmission of fluid pressureWhenever external pressure is applied on any part of a fluid contained in a vessel, it is transmitted undiminished and equally in all directions.Hydraulic lift and hydraulic brakes are based on the Pascal’s law.
F2 = PA2 = F1A1/A2
10.3 STREAMLINE FLOW
Streamline Flow is a steady flow of liquid, in which each particle of liquid follows the same path and the same velocity as that of its predecessor.(The path taken by a fluid particle under a steady flow is called a streamline)Critical velocity : Streamline flow is possible only when, velocity of flow is less than a limiting value. This velocity is called critical velocity.
Equation of continuity
Consider streamline flow of a liquid of density ‘ρ’ through a pipe of different area of cross section.[ Note: Mass = Volume × ρ = (Area × Length) × ρ ]Mass of fluid flowing in through the large area ‘A1’ in a time ‘Δt’ is given byM1 = A1 × (v1 Δt ) × ρMass of fluid flowing out through the small area ‘A2’ in a time ‘Δt’ is given byM2 = A2 × ( v2 Δt ) × ρFluid mass flowing in = Fluid mass flowing outA1 × (v1 Δt ) × ρ = A2 × ( v2 Δt ) × ρA1v1 = A2v2
Av = constantThis equation is called Equation of Continuity
Turbulent flow
when velocity of flow is greater than the critical velocity, the liquid flowbecomes disorderly and zigzag and is called turbulent flow.
10.4 BERNOULLI’S PRINCIPLE
The work done on the fluid at left end (BC) is W1 = P1A1(v1Δt) = P1ΔVThe work done by the fluid at the other end (DE) is W2 = P2A2(v2Δt) = P2ΔVThe total work done on the fluid is W1 – W2 = (P1− P2) ΔV
Part of this work goes into changing the kinetic energy of the fluid, and part goes into changing the gravitational potential energy
10.4 BERNOULLI’S PRINCIPLE
change in gravitational potential energy is ΔU = ρgΔV (h2 − h1)The change in its kinetic energy is
employing the work – energy theorem
We now divide each term by ΔV to obtain
This is Bernoulli’s equation
BERNOULLI’S THEOREM
The sum of pressure energy, kinetic energy, and potential energy per unit mass is always constant for the streamline flow of a non-viscous and incompressible fluid
10.4.1 Speed of Efflux: Torricelli’s Law
Torricelli ‘s LawThe speed of efflux (fluid outflow) from an open tank is given by a formula identical to that of a freely falling body
According to equation of continuity
Since A2 >> A1,v2 = 0 (fluid at rest) Applying Bernoulli’s theorem
10.4.1 Speed of Efflux: Torricelli’s Law
Applying Bernoulli’s theorem
P1 =Pa (atmospheric pressure)y2 − y1 = h (shown in the figure)
10.4.2 Venturi-meter
It is a gauge used to measure the rate of flow of fluid when fluid is steady
Speed at the constriction (Using equation of continuity)
According to Bernoulli’s equation
Speed of the fluid at the wide neck
10.4.3 BLOOD FLOW AND HEART ATTACK
•Accumulation of plaque constricts the artery.•To drive blood through it, the activity of heart increases.•Speed of blood in the region increases, lowering the inside pressure of artery.•Artery may collapse due to high external pressure.•Heart exerts further pressure and opens the artery to force the blood through it.•Blood rushes through the opening and the internal pressure of artery drops.•This leads to repeat collapse and results in heart attack
10.4.4 DYNAMIC LIFT
•Aerofoil or lift on aircraft wing
Wings of aeroplane look similar to an aerofoil.Aerofoil moving against the wind causes the streamline to crowd more above the wing than below it.Therefore, the speed on top is more than it is below it.Upward force resulting in a dynamic lift of wings balances the weight of the plane
10.5 VISCOSITY
It is the resistance of the fluid motion. This force exists when there is relative motion between the layers of liquid
Laminar − For any layer of liquid, its upper layer pulls it forward while lower layer pulls it backward. This results in force between the layers. This type of flow is known as laminar
10.5 VISCOSITY
Co-efficient of viscosity,
Shearing stress =
Strain rate =
•Unit of viscosity is poiseiulle (Pl) or Nsm−2 or Pa s.•Thin liquids are less viscous than thick liquids.•Viscosity of liquids decreases with temperature while it increases in case of gases.
Stoke’s Law
An object moving through a fluid drags the liquid in contact. This force between the layers of the fluid makes the body experience a retarding force.Retarding force (F) depends onvelocity of the object (v)viscosity of the fluid (η)radius of the sphere (a)
∴ F = 6πηavThis is known as Strokes’ law
Terminal Velocity (vt)
When a spherical body falls through a viscous fluid, it experiences a viscous force. The magnitude of viscous force increases with the increase in velocity of the falling body under the action of its weight. As a result, the viscous force soon balances the driving force (weight of the body) and the body starts moving with a constant velocity known as its terminal velocity
Using Strokes’ law
Where,ρ − Mass density of sphereσ − Mass density of fluidTerminal velocity
10.6 REYNOLDS NUMBER
When the rate of flow of a fluid is large, the flow becomes turbulent. An obstacle placed in the path of a fast moving fluid causes turbulence
Reynolds (Re) number implies if the flow would be turbulent or not
Re =
Where,ρ − Density of fluidd − Dimension of pipev − Speed of fluid flowη − Viscosity of the fluid
10.6 REYNOLDS NUMBER
Re is dimensionless.Re < 1000 [Streamline or laminar flow]2000 ≥ Re ≥ 1000 [Unsteady flow]Re > 2000 [Turbulent flow]
Re is ratio of inertial force to viscous force.
Use − Turbulence promotes mixing; increases the transfer rate of mass, momentum, and energy.
10.7 SURFACE TENSION
10.7 SURFACE TENSION
The Surface tension is the property by virtue of which the free surface of a liquid behaves like elastic stretched membrane tending to contract.Surface tension (S) is measured as the tangential force (due to the surface molecules) per unit length.Surface Tension(S) = Force / Length.Its unit is N/m.
10.7.1 Surface Energy
Surface of a liquid acts as a stretched membrane. So molecules in this layer posses’ elastic potential energy. This elastic potential energy is called surface energy.Also Surface Energy = Work done / surface Area
10.7.2 Surface Energy and Surface Tension
Consider a rectangle; the side ‘AB’ is movable. Dip the frame in a soap solution; then due to surface tension ‘AB’ moves through a distance ‘b’..: Work done = Tangential Force × bBut, Tangential Force = Surface Tension (S) × 2l .This is because; surface tension is acting on the upper surface and lower surface of the soap film.Tangential Force = S ×2 lWork done = S × 2l ×bSurface Energy = Work done /Area
Numerically, Surface Energy = Surface Tension
10.7.3 Angle of Contact
Angle between tangent to the liquid surface at the point of contact and solid surface inside the liquid is called angle of contact.
10.7.4 Drops and Bubbles
r − Radius of dropP0 − Pressure outside the bubblePi − Pressure inside the bubbleS − Surface tension of the bubble
Surface energy = 4πr2SLet radius increase by Δ r.Then, extra surface energy = [4 π (r + Δr)2 − 4πr2] S
= 8πrΔrS (1)
Energy gain in the pressure difference Pi − P0
Work done, ∴ W = (Pi − P0) 4πr2Δr (2)At equilibrium, the energy used is balanced by the energy gained.From equations (1) and (2),(Pi − P0) = 2S/r
For Bubbles, having two interfaces(Pi − P0) = 2S/r
10.7.5 Capillary Rise
10.7.5 Capillary Rise
Angle of contact between water and glass is acute.Surface of water in the capillary is concave.Pressure difference between two sides of top surface, Pa − P0 = 2S/r
Considering points A and B, they must be at same pressure i.e.,P0 + hρg = Pa
Therefore, capillary rise is due to surface tension.
Height of water rise, (θ=00)
10.7.6 Detergents and Surface Tension
Ordinary water will not remove greasy dirt. This is because water could not wet greasy dirt.When we add detergent, small glob of dirt can be captured by detergent molecule by surrounding it.This ‘new system molecules’ can be captured or wet by water molecules. So they can be removed