# DARSHAN INSTITUTE OF ENGINEERING AND TECHNOLOGY, RAJKOT FLUID MECHANICS ( )

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1 DARSHAN INSTITUTE OF ENGINEERING AND TECHNOLOGY, RAJKOT FLUID MECHANICS ( ) Sr. No. Experiment Start Date End Date Sign Remark 1. To understand pressure measurement procedure and related instruments/devices. 2. To determine the Metacentric height of a given floating body. 3. To validate Bernoulli s Theorem as applied to the flow of water in a tapering circular duct. 4. To measure the velocity of flow using Pitot tube To determine the Coefficient of discharge through different flow meters. (Orifice meter, Venturimeter Nozzle meter and Rotameter) To determine the Coefficient of discharge through open channel flow over a Notch. (Rectangular, Triangular and Trapezoidal Notch) 7. To determine the different types of flow Patterns by Reynolds s experiment. 8 To determine the Friction factor for the different pipes. 9 To determine the loss coefficients for different pipe fittings.

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3 EXPERIMENT NO. 1 Pressure Measurement Date: / / Objective To study pressure and pressure measurement devices. Introduction Fluid pressure can be defined as the measure of force per-unit-area exerted by a fluid, acting perpendicularly to any surface it contacts The standard SI unit for pressure measurement is the Pascal (Pa) which is equivalent to one Newton per square meter (N/m2) or the Kilopascal (kpa) where 1 kpa = 1000 Pa. Pressure can be expressed in many different units including in terms of a height of a column of liquid. The Table below lists commonly used units of pressure measurement and the conversion between the units. Pressure measurements can be divided into three different categories: absolute pressure, gage pressure and differential pressure. Absolute pressure refers to the absolute value of the force per-unit-area exerted on a surface by a fluid. Therefore the absolute pressure is the difference between the pressure at a given point in a fluid and the absolute zero of pressure or a perfect vacuum. Gauge pressure is the measurement of the difference between the absolute pressure and the local atmospheric pressure. Local atmospheric pressure can vary depending on ambient temperature, altitude and local weather conditions. A gage pressure by convention is always positive. A negative gage pressure is defined as vacuum. Vacuum is the measurement of the amount by which the local atmospheric pressure exceeds the absolute pressure. A perfect vacuum is zero absolute pressure. Figure below shows the relationship between absolute, gage pressures and vacuum. 1-1

4 Pressure Measurement Relationship between various pressure measurement devices Differential pressure is simply the measurement of one unknown pressure with reference to another unknown pressure. The pressure measured is the difference between the two unknown pressures. This type of pressure measurement is commonly used to measure the pressure drop in a fluid system. Since a differential pressure is a measure of one pressure referenced to another, it is not necessary to specify a pressure reference. For the English system of units this could simply be psi and for the SI system it could be kpa. In addition to the three types of pressure measurement, there are different types of fluid systems and fluid pressures. There are two types of fluid systems; static systems and dynamic systems. As the names imply, a static system is one in which the fluid is at rest and a dynamic system is on in which the fluid is moving. Pressure Measurement Devices Manometer A Manometer is a device to measure pressures. A common simple manometer consists of a U shaped tube of glass filled with some liquid. Typically the liquid is mercury because of its high density. In the figure to the right we show such a U shaped tube filled with a liquid. Note that both ends of the tube are open to the atmosphere. Thus both points A and B are at atmospheric pressure. The two points also have the same vertical height 1-2

5 Pressure Measurement Now the top of the tube on the left has been closed. We imagine that there is a sample of gas in the closed end of the tube. The right side of the tube remains open to the atmosphere. The point A, then, is at atmospheric pressure. The point C is at the pressure of the gas in the closed end of the tube. The point B has a pressure greater than atmospheric pressure due to the weight of the column of liquid of height h. The point C is at the same height as B, so it has the same pressure as B. And this is equal to the pressure of the gas in the closed end of the tube. Thus, in this case the pressure of the gas that is trapped in the closed end of the tube is greater than atmospheric pressure by the amount of pressure exerted by the column of liquid of height h. Some "rules" to remember about U-tube manometry Manometer height difference does not depend on tube diameter. Manometer height difference does not depend on tube length. Manometer height difference does not depend on tube shape. Shape of a container does not matter in hydrostatics. This implies that a U-tube manometer does not have to be in a perfect U shape. There is a way to take advantage of this, namely one can construct an inclined manometer, as shown here. Although the column height difference between the two sides does not change, an inclined manometer has better resolution than does 1-3

6 Pressure Measurement a standard vertical manometer because of the inclined right side. Specifically, for a given ruler resolution, one "tick" mark on the ruler corresponds to a finer gradation of pressure for the inclined case. Burdon Pressure Gauge A Bourdon gauge uses a coiled tube, which, as it expands due to pressure increase causes a rotation of an arm connected to the tube. In 1849 the Bourdon tube pressure gauge was patented in France by Eugene Bourdon. Parts of Burdon tube The pressure sensing element is a closed coiled tube connected to the chamber or pipe in which pressure is to be sensed. As the gauge pressure increases the tube will tend to uncoil, while a reduced gauge pressure will cause the tube to coil more tightly. This motion is transferred through a linkage to a gear train connected to a pointer. The pointer is presented in front of a card face is inscribed with the pressure indications associated with particular pointer deflections. Apparatus Description The manometers and gauges unit is a framed structure with a backboard, holding a: Vertical U-tube manometer U-tube manometer with an inclined limb Bourdon gauge for measuring vacuums Bourdon gauge for measuring positive pressure, and 1-4

7 Pressure Measurement Syringe assembly for pressurizing and reducing pressure in the measurement devices. Each gauge and manometer has a delivery point to connect to the syringe using plastic tubing (included). All connections are push-fit, and T-pieces are provided to enable two instruments to be connected to one point. Experimental Procedure 1. Using the syring connects its plastic tubing to Pressure gauge. Push the syring arm to generate pressure. Observe the deflection on the gauge 2. Now connect the syring tubing to vacuum gauge. Release the arm of syring to generate vacuum and observe the change in deflection. 3. U tube Manometer can be connected to any of the flow meter devices. Switch the pump and observe the change in mercury levels in the manometer. Calculate the pressure difference. 4. Similarly connect the Inclined U tube manometer to any of the flow meter and calculate pressure difference Observations: Density of liquid flowing in pipe = Density of liquid flowing in pipe = Sr. No. Type of Manometer Manometric Reading h1 h2 1 U tube Manometer 2 Inclined Tube Manometer 3 Pressure Gauge 4 Vacuum Gauge Pressure/Pressure Difference Calculations 1-5

8 Pressure Measurement In the above figure, since the pressure at the height of the lower surface of the manometer fluid is the same in both arms of the manometer, we can write the following equation: P 1 + ρ 1 gd 1 = P 2 + ρ 2 gd 2 + ρ f g h Here, ρ 1 = ρ 2 = ρ w = Density of water; P 1 - P 2 = ρ w gd 2 + ρ f g h ρwgd 1 Also d 1 - d 2 = h P 1 - P 2 = (ρ f - ρ w ) g h Here ρ f = Density of Mercury; Substituting Standard Values P1-P2 = (kg/m 3 ) x g (m/s 2 ) x h/1000 (m) = g h (in N/m 2 ) Where g =9.81 m/s 2 ; h in mm Conclusion

9 EXPERIMENT NO. 2 Metacentre Date: / / Objective To determine the Metacentric height of a given floating body. Introduction Buoyancy When a body is completely submerged in a fluid, or it is floating or partially submerged, the resultant fluid force acting on the body is called the buoyant force. It is also known as the net upward vertical force acting on the body. A net upward vertical force results because pressure increases with depth and the pressure forces acting from below are larger than the pressure forces acting above. The Center of buoyancy is the center of gravity of the displaced water. It lies at the geometric center of volume of the displaced water. Metacentre For the investigation of stability of floating body, it is necessary to determine the position of its metacentre with respect to its centre of gravity. Consider a floating ship model, the weight of the ship acts through its centre of gravity and is balanced by an equal and opposite buoyant force acting upwards through the centre of buoyancy i.e. the centre of gravity of liquid displaced by the floating body. A small angular displacement shifts the centre of buoyancy and the intersection of the line of action of the buoyant force passing through the new centre of buoyancy and the extended line would give the metacentre. The distance between centre of gravity (G) and metacentre (M) is known as Metacentric height (GM). 2-1

10 Metacentre There are three conditions of equilibrium of a floating body 1. Stable Equilibrium - Metacentre lies above the centre of gravity 2. Unstable Equilibrium- Metacentre lies below the centre of gravity 3. Neutral Equilibrium - Metacentre coincides with centre of gravity The Metacentric height (GM) is given by GM = Where, W = weight of the floating body m = movable weight (m x X) (W x tanθ) X = distance through which the movable load is shifted = Angle of Heel Apparatus Description The apparatus consist of a SS tank and is provided with a drain cock. The floating body is made from Clear Transparent Acrylic. It is provided with movable weights, protractor to measure the angle of Heel and pointer. Weights are also provided to increase the weight of floating body by known amount. Experimental Procedure 1. Fill the SS tank to about 2/3 levels 2. Place the floating body in the tank. 3. Apply momentum to the floating body by moving one of the adjustable weights (m) through a known distance. 4. Note down the angle of heel corresponding to this shifts of weight with the help of protractor and pointer. 5. Take about 4-5 such readings by changing the position of the adjustable weight and find out centre of gravity in each case Observation Table: Weight of the ship model = 1.5 X 9.81 = N Given Movable Weights = 100 gm; 50 gm = N; N 2-2

11 Metacentre Sr. No. Movable Weight (m) N Distance moved (X) M Angle of Tilt Tan Metacentric Height GM M Calculations Metacentric height GM = (m x X) (W x tanθ) Conclusion

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13 EXPERIMENT NO. 3 Bernoulli s Theorem Date: / / Objective To validate Bernoulli s Theorem as applied to the flow of water in a tapering circular duct. Introduction Bernoulli's principle is named after the Dutch-Swiss mathematician Daniel Bernoulli who published his principle in his book Hydrodynamica in Bernoulli s principle in its simplest form states that "the pressure of a fluid [liquid or gas] decreases as the speed of the fluid increases." The principle behind Bernoulli s theorem is the law of conservation of energy. It states that energy can be neither created nor destroyed, but merely changed from one form to another. The energy, in general, may be defined as the capacity to do work. Though the energy exists in many forms, yet the following are important from the subject point of view: 1. Potential Energy 2. Kinetic Energy and 3. Pressure Energy Potential energy of a Liquid in Motion It is the energy possessed by a liquid particle, by virtue of its position. If a liquid particle is Z meters above the horizontal datum (arbitrary chosen), the potential energy of the particle will be Z meter-kilogram (briefly written as mkg) per kg of liquid. Potential head of the liquid, at that point, will be Z meters of the liquid. Kinetic Energy of a liquid Particle in Motion It is the energy, possessed by a liquid particle, by virtue of its motion or velocity. If a liquid particle is flowing with a mean velocity of v meter per second, then the kinetic energy of the particle will be v2/2g meter of the liquid. Velocity head of the liquid, at that velocity, will be v2/2g meter of liquid. Pressure Energy of a liquid Particle in Motion It is the energy, possessed by a liquid particle, by virtue of its existing pressure. If a liquid particle is under a pressure of p kg/m2, then the pressure energy of the particle will be p/w 3-1

14 Bernoulli s Theorem mkg per kg of liquid, where w is the specific weight of the liquid. Pressure head of the liquid under that pressure will be p/w meter of the liquid. Total Energy of a liquid Particle in Motion The total energy of a liquid particle, in motion, is the sum of its potential energy, kinetic energy and pressure energy. Mathematically, Total Energy, E = P w + v2 m kg + Z in 2g kg of liquid Bernoulli s Equation It states, For a perfect incompressible liquid, flowing in a continuous stream, the total energy of a particle remains the same; while the particle moves from one point to another. This statement is based on the assumption that there are no losses due to friction in pipe. Mathematically, Total Energy, E = P w + v2 2g + Z = Constant Apparatus Description The apparatus is made from transparent acrylic and has both the convergent and divergent sections. Water is supplied from the constant head tank attached to the test section. Constant level is maintained in the supply tank. Piezometric tubes are attached at different distance on the test section. Water discharges to the discharge tank attached at the far end of the test section and from there it goes to the measuring tank through valve. The entire setup is mounted on a stand. Experimental Procedure 1. Note down the area of cross-section of the conduit at sections where piezometers have been fixed. 2. Open the supply valve and adjust the flow in the conduit so that the water level in the inlet tank remains at a constant level (i.e., the flow becomes steady) 3. Measure the height of water level (above an arbitrarily selected suitable horizontal plane) in different piezometer tubes. 4. Measure the discharge by calculating time taken for L liters flow. 5. Repeat steps (2) to (4) for other discharges. 3-2

15 Observation Table Bernoulli s Theorem Piezometer tube number Area of cross-section, A Distance of piezometer from tank Run No.1 Discharge Q 1 = L/ t Run No.1 Discharge Q 2 = L/ t Run No.1 Discharge Q 3 = L/ t V=Q/A V 2 /2g (p/ρg) + z E V=Q/A V 2 /2g (p/ρg) + z E V=Q/A V 2 /2g (p/ρg) + z E Plot the following on an ordinary graph paper for all the runs taken. 1. {( p ) + z} V/s distance (x) of piezometer tubes from some reference point. ρg Draw a smooth curve passing through the plotted points. This is known as the hydraulic gradient line. 2. E = {( p ρg ) + z + V2 2g } V/s distance (x) of piezometer tubes on the graph {(p/ρg) + z} v/s distance. Draw a smooth curve passing through the plotted points. This is the total energy line. Conclusion

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17 EXPERIMENT NO. 4 Pitot Tube Date: / / Objective To study and measure velocity of flow using Pitot tube Introduction A Pitot tube is a pressure measurement instrument used to measure fluid flow velocity. The pitot tube was invented by the French engineer Henri Pitot in the early 1700s and was modified to its modern form in the mid 1800s by French scientist Henry Darcy. It is widely used to determine the airspeed of an aircraft and to measure air and gas velocities in industrial applications. The basic pitot tube consists of a tube pointing directly into the fluid flow. As this tube contains fluid, a pressure can be measured; the moving fluid is brought to rest (stagnates) as there is no outlet to allow flow to continue. This pressure is the stagnation pressure of the fluid, also known as the total pressure or (particularly in aviation) the pitot pressure. The measured stagnation pressure cannot of itself be used to determine the fluid velocity (airspeed in aviation). However, Bernoulli's equation states: Stagnation pressure = static pressure + dynamic pressure Mathematically this can also be written: Solving that for velocity we get: Where, V is fluid velocity Pt is stagnation or total pressure Ps is static pressure; P t = P S + ( V2 2g ) V = 2g (P t P s ) 4-1

18 Pitot Tube The dynamic pressure, then, is the difference between the stagnation pressure and the static pressure. Apparatus Description The setup consist of simple clear Perspex channel with two tube each to measure static and stagnation pressure of the fluid in the channel. Channel is supplied water with the help of tank and the flow is controlled by a gate valve. Scale is imprinted next to the tube to measure the pressure heads. Experimental Procedure 1. Switch on the pump and feel the tank that supplies water to the pitot apparatus. 2. Now slowly open the pitot outlet valve so that channel is filled completely with water 3. Observe and note down the pressure heads reading in m of water 4. Calculate time for discharge for known quantity of water 5. Calculate and compare theoretical and actual velocities Observations Table Area of flow Channel = 0.03 m Sr. No. Pt (m) Ps (m) (Pt-Ps) (m) Vpitot m/s Time s Q m 3 /s Vmeasured m/s Calculations Area of flow Channel = 0.03 m 2 V = 2g (P t P s ) Conclusion

19 Orifice Meter,Venturi meter, Nozzle meter, Rotameter EXPERIMENT NO. 5 Date: / / Objective To determine the co-efficient of discharge through Orifice meter, Venturimeter, Nozzle meter and Rotameter. Orifice Meter Introduction The most important class of flow meter is that in which the flow is either accelerated or retarded at the measuring sections by reducing the flow area, and the change in the kinetic energy is measuring sections by reducing the flow area and the change in the kinetic energy is measured by recording the pressure difference produced. This class includes orifice meter. A circular Opening in a plate which is fitted suitably in a pipeline is a simple device to measure the discharge flowing in the pipeline. Such a device is known as orifice meter and is as shown in the figure. the opening is normally at the centre of the plate as shown in figure. Applying Bernoulli's equation between section 1 and 2 and using continuity equation, it can be shown that, Q act = Cd. a 2 2g(h 1 h 2 ) Where, A 2 = Area of cross section of the orifice 1 ( a 2 a 1 ) 2 (h 1 h 2 ) = Difference in the piezometeric heads at section 1 and 2 Apparatus Description Simple orifice meter Orifice meter is mounted along a pipeline with sufficient distance to stabilize flow between two meters. The pressure taps are provided at sections as given in the fig. Pressure head difference between sections can be read on manometer having mercury as the manometer fluid. A valve, fitted at the end of the pipeline, is used for regulating the discharge in the pipeline. 5-1

20 Orifice Meter,Venturi meter, Nozzle meter, Rotameter Technical Specifications Orifice meter: Size = 26 mm Orifice Size = 16 mm Dia Ratio = 0.6 Experimental Procedure 1. Fill the storage tank/sump with the water. 2. Switch on the pump and keep the control valve fully open and close the bypass valve to have maximum flow rate through the meter. 3. Open control valve of the orifice meter. 4. Open the vent cocks provided at the top of the manometer to drive out the air from the manometer limbs and close both of them as soon as water start coming out. 5. Note down the difference of level of mercury in the manometer limbs. 6. Keep the drain valve of the collection tank closed till it s time to start collecting the water. 7. Close the drain valve of the collection tank and note down the initial level of the water in the collection tank. 8. Collect known quantity of water in the collection tank and note down the time required for the same. 9. Change the flow rate of water through the meter with the help of control valve and repeat the above procedure. 10. Take about 2-3 readings for different flow rates. Observations For Orifice meter: Diameter at inlet D 1 = 26 mm; Area A 1 = 5.31 x 10-4 m 2 Diameter at orifice D 2 = 16 mm; Area A 2 = 2.01 x 10-4 m 2 Sr. No Manometer Difference In mm of Hg Flow rate (time for L liters) t in sec

21 Calculations Actual Discharge, As per theory, Q act = Orifice Meter,Venturi meter, Nozzle meter, Rotameter L time required to collect L ltrs of water in m3 /sec Q th = Cd. a 2 2g(h 1 h 2 ) 1 ( a 2 a 1 ) 2 Before Substituting Values of Q act and (h1 h2) into the above equation, it will simpler to establish the value of = a 2 2g 1 ( a = = x x9.81 = 9.65 x a ) Q act = Cd x 9.65x 10 4 x (h 1 h 2 ) Cd = x Q act (h 1 h 2 ) Put the values of Q and (h 1 - h 2 ) from observations Cd =.. Venturi Meter Introduction The most important class of flow meter is that in which the flow is either accelerated or retarded at the measuring sections by reducing the flow area, and the change in the kinetic energy is measuring sections by reducing the flow area and the change in the kinetic energy is measured by recording the pressure difference produced. This class includes Venturimeter Venturimeter is used for the measurement of discharge in a pipeline. Since head loss caused due to installation of venturi meter in a pipeline is less than that caused due to installation of orficemeter, the former is usually preferred particularly for higher flow rates. A venturimeter consists of a converging tube which is followed by a diverging tube. The junction of the two is termed as 'throat' which is the section of minimum cross-section. 5-3

22 Orifice Meter,Venturi meter, Nozzle meter, Rotameter Venturi Meter Apparatus Description Venturimeter is mounted along a pipeline with sufficient distance to stabilize flow between two meters. The pressure taps are provided at sections as given in the fig. Pressure head difference between sections can be read on manometer having mercury as the manometer fluid. A valve, fitted at the end of the pipeline, is used for regulating the discharge in the pipeline. Technical Specifications Venturimeter Size = 26 mm Throat Size = 16 mm Dia Ratio = 0.6 Experimental Procedure 1. Fill the storage tank/sump with the water. 2. Switch on the pump and keep the control valve fully open and close the bypass valve to have maximum flow rate through the meter. 3. Open control valve of the venturimeter. 4. Open the vent cocks provided at the top of the manometer to drive out the air from the manometer limbs and close both of them as soon as water start coming out. 5. Note down the difference of level of mercury in the manometer limbs. 6. Keep the drain valve of the collection tank closed till its time to start collecting the water. 7. Close the drain valve of the collection tank and note down the initial level of the water in the collection tank. 5-4

23 Orifice Meter,Venturi meter, Nozzle meter, Rotameter 8. Collect known quantity of water in the collection tank and note down the time required for the same. 9. Change the flow rate of water through the meter with the help of control valve and repeat the above procedure. 10. Take about 2-3 readings for different flow rates. Observations For Venturimeter, Diameter at inlet D 1 = 26 mm; Area A 1 = 5.31 x 10-4 m 2 Diameter at throat D 2 = 16 mm; Area A 2 = 2.01 x 10-4 m 2 Sr. No Manometer Difference In mm of Hg Flow rate (time for 10 lit) t in sec Calculations Actual Discharge, As per theory, Q act = 0.01 time required to collect 10 ltrs of water in m3 /sec Q act = Cd. a 2 2g(h 1 h 2 ) 1 ( a 2 a 1 ) 2 Before Substituting Values of Q act and (h1 h2) into the above equation, it will simpler to establish the value of = a 2 2g 1 ( a = = x x9.81 = 9.65 x a ) Q act = Cd x 9.65x 10 4 x (h 1 h 2 ) Cd = x Q act (h 1 h 2 ) Put the values of Q and (h 1 - h 2 ) from observations Cd =.. 5-5

24 Orifice Meter,Venturi meter, Nozzle meter, Rotameter Nozzle meter Introduction The most important class of flow meter is that in which the flow is either accelerated or retarded at the measuring sections by reducing the flow area, and the change in the kinetic energy is measuring sections by reducing the flow area and the change in the kinetic energy is measured by recording the pressure difference produced. This class includes Nozzle meter. The flow nozzle is a venturi meter that has been simplified and shortened by eliminating the gradual downstream expansion. The streamlined entrance of the nozzle causes a straight jet without contraction, so its effective discharge coefficient is nearly the same as the venturi meter. Flow nozzles allow the jet to expand of its own accord. The flow nozzle costs less than venturimeter. It has the disadvantage that the overall losses are much higher because of the lack of guidance of the jet downstream from the nozzle opening. Simple nozzle meter Apparatus Description Nozzle meter is mounted along a pipeline with sufficient distance to stabilize flow between two meters. The pressure taps are provided at sections as given in the fig. Pressure head difference between sections can be read on manometer having mercury as the manometer fluid. A valve, fitted at the end of the pipeline, is used for regulating the discharge in the pipeline. 5-6

25 Technical Specifications Nozzle meter: Size = 26 mm Nozzle Size = 16 mm Dia Ratio = 0.6 Orifice Meter,Venturi meter, Nozzle meter, Rotameter Experimental Procedure 1. Fill the storage tank/sump with the water. 2. Switch on the pump and keep the control valve fully open and close the bypass valve to have maximum flow rate through the meter. 3. Open control valve of the nozzle meter. 4. Open the vent cocks provided at the top of the manometer to drive out the air from the manometer limbs and close both of them as soon as water start coming out. 5. Note down the difference of level of mercury in the manometer limbs. 6. Keep the drain valve of the collection tank closed till it s time to start collecting the water. 7. Close the drain valve of the collection tank and note down the initial level of the water in the collection tank. 8. Collect known quantity of water in the collection tank and note down the time required for the same. 9. Change the flow rate of water through the meter with the help of control valve and repeat the above procedure. 10. Take about 2-3 readings for different flow rates. Observations For Nozzle meter: Diameter at inlet D 1 = 26 mm; Area A 1 = 5.31 x 10-4 m 2 Diameter at orifice D 2 = 16 mm; Area A 2 = 2.01 x 10-4 m 2 Sr. No Manometer Difference In mm of Hg Flow rate (time for 10 lit) t in sec

26 Orifice Meter,Venturi meter, Nozzle meter, Rotameter Calculations Actual Discharge, As per theory, Q act = 0.01 time required to collect 10 ltrs of water in m3 /sec Q th = Cd. a 2 2g(h 1 h 2 ) 1 ( a 2 a 1 ) 2 Before Substituting Values of Qact and (h1 h2) into the above equation, it will simpler to establish the value of = a 2 2g 1 ( a = = x x9.81 = 9.65 x a ) Q act = Cd x 9.65x 10 4 x (h 1 h 2 ) Cd = x Q act (h 1 h 2 ) Put the values of Q and (h1 - h2) from observations Cd =.. Rota meter Introduction The most important class of flow meter is that in which the flow is either accelerated or retarded at the measuring sections by reducing the flow area, and the change in the kinetic energy is measuring sections by reducing the flow area and the change in the kinetic energy is measured by recording the pressure difference produced. This class includes rotameter. The rotameter is an industrial flow meter used to measure the flow rate of liquids and gases. The rotameter consists of a tube and float. The float response to flow rate changes is linear. The rotameter is popular because it has a linear scale, a relatively long measurement range, and low pressure drop. It is simple to install and maintain. The rotameter's operation is based on the variable area principle: fluid flow raises a float in a tapered tube, increasing the area for passage of the fluid. The greater the flow, the higher the float is raised. The height of the float is directly proportional to the flow rate. With liquids, 5-8

27 Orifice Meter,Venturi meter, Nozzle meter, Rotameter the float is raised by a combination of the buoyancy of the liquid and the velocity head of the fluid. With gases, buoyancy is negligible, and the float responds to the velocity head alone. S= Flow Force A = Buoyancy G= Gravity Rota meter Apparatus Description Rota meter is mounted along a pipeline with sufficient distance to stabilize flow between two meters. The pressure taps are provided at sections as given in the fig. Pressure head difference between sections can be read on manometer having mercury as the manometer fluid. A valve, fitted at the end of the pipeline, is used for regulating the discharge in the pipeline. Technical Specifications Rota meter: Size = LPH Type = Thread Ends Experimental Procedure 1. Fill the storage tank/sump with the water. 2. Switch on the pump and keep the control valve fully open and close the bypass valve to have maximum flow rate through the meter. 3. Verify the rotameter readings flow marking provided by manufacturer. 4. Take about 2-3 readings for different flow rates. 5-9

28 Orifice Meter,Venturi meter, Nozzle meter, Rotameter Observations Sr. No Rota meter Scale (in LPH) Flow rate (time for 10 lit) t in sec Calculations Actual discharge, Q act = Discharge in LPH = Q act x L time required to collect L ltrs of water in m3 /sec Conclusion

29 EXPERIMENT NO. 6 Notches Date: / / Objective To calibrate the given Rectangular, Triangular and Trapezoidal Notches Introduction Measurement of flow in open channel is essential for better management of supplies of water. Hydraulic structures such as weirs are emplaced in the channel. They are used to determine the discharge indirectly from measurements of the flow depth. A notch is an opening in the side of a measuring tank or reservoir extending above the free surface. A weir is a notch on a large scale, used, for the measurement of discharge in free surface flows like a river. A weir is an orifice placed at the water surface so that the head on its upper edge is zero. Hence, the upper edge can be eliminated, leaving only the lower edge named as weir crest. A weir can be of different shapes - rectangular, triangular, trapezoidal etc. A triangular weir is particularly suited for measurement of small discharges. Rectangular Notch The discharge over an unsubmerged rectangular sharp-crested notch is defined as: Q = 2 3 Cd. L. 2g H3 2 Triangular Notch \ Rectangular notch The rate of flow over a triangular weir mainly depends on the head H, relative to the crest of the notch; measured upstream at a distance about 3 to 4 times H from the crest. For triangular notch with apex angle, the rate of flow Q is obtained from the equation, Q = 8 15 Cd 2g tan θ 2 H

30 Notches Here, Cd is termed the coefficient of discharge of triangular notch Triangular Notch Trapezoidal Notch Also known as Cipolletti weirs are trapezoidal with 1:4 slopes to compensate for end contraction losses. The equation generally accepted for computing the discharge through an unsubmerged sharp-crested Cipolletti weir with complete contraction is: Q = Cd. L. H 3 2 Where, Q = Discharge over notch (m 3 /sec) L = Bottom of notch width H = Head above bottom of opening in meter Apparatus Description Trapezoidal notch The pump sucks the water from the sump tank, and discharges it to a small flow channel. The notch is fitted at the end of channel. All the notches and weirs are interchangeable. The water flowing over the notch falls in the collector. Water coming from the collector is directed to the measuring tank for the measurement of flow. The following notches are provided with the apparatus: 1. Rectangular notch (Crest length L = 0.050m) 2. Triangular notch (Notch Angle 60 0 ) 3. Trapezoidal notch (Crest length L = 0.075m; Slope = 4V:1H) 6-2

31 Notches (1) (2) (3) Experimental Procedure: 1. Fit the required notch in the flow channel. 2. Fill up the water in the sump tank. 3. Open the water supply gate valve to the channel and fill up the water in the channel up to sill level. 4. Take down the initial reading of the crest level (sill level) 5. Now start the pump and open the gate valve slowly so that water starts flowing over the notch 6. Let the water level become stable and note down the height of water surface at the upstream side by the sliding depth gauge. 7. Close the drain valve of measuring tank, and measure the discharge. 8. Take the reading for different flow rates. 9. Repeat the same procedure for other notch also. Observations: Notch Type: Triangular Sr. No Still level reading s in meters Water height on upstream side h in meters Discharge time for L liters t in second 6-3

32 Notches Notch Type: Rectangular Sr. No Still level reading s in meters Water height on upstream side h in meters Discharge time for L liters t in second Notch Type: Trapezoidal Sr. No Still level reading s in meters Water height on upstream side h in meters Discharge time for L liters t in second Calculations: Rectangular Notch 1. Head over the notch, H = (h s) in meter 2. Actual Discharge, Q act = L t in m3 /sec 3. Crest length of notch = 0.05 m 4. Theoretical discharg, Q th = 2 3 L. 2g H3 2 in m 3 /sec 5. Coefficient of discharge Cd = Q act Q th Triangular notch 1. Head over the notch, H = (h s) in meter 6-4

33 2. Actual Discharge, Q act = Crest length of notch = m t in m 3 /sec Notches 4. Theoretical discharg, Q th = g tan 60 2 H5 2 in m 3 /sec 5. Coefficient of discharge Cd = Q act Q th Trapezoidal Notch (or Cipolletti Weir) 1. Head over the notch, H = (h s) in meter 2. Actual Discharge, Q act = Crest length of notch = m t in m 3 /sec 4. Theoretical discharg, Q th = L. H 3 2 in m 3 /sec 5. Coefficient of discharge Cd = Q act Q th Conclusion:

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35 EXPERIMENT NO. 7 Reynolds s Apparatus Date: / / Objective To study Laminar and Turbulent Flow and It s visualization on Reynolds s Apparatus Introduction The properties of density and specific gravity are measures of the heaviness of fluid. These properties are however not sufficient to uniquely characterize how fluids behave since two fluids (such as water and oil) can have approximately the same value of density but behaves quite differently when flowing. There is apparently some additional property that is needed to describe the fluidity of the fluid. Viscosity is defined as the property of a fluid which offers resistance to the movement of one layer of fluid over another adjacent layer of the fluid. It is an inherent property of each fluid. Its effect is similar to the frictional resistance of one body sliding over other body. As viscosity offers frictional resistance to the motion of the fluid consequently. In order to maintain the flow, extra energy is to be supplied to overcome effect of viscosity. The frictional energy generated comes out in form of heat and dissipated to the atmosphere through boundary surfaces. Types of flow Laminar flow Laminar flow is that type of flow in which the particle of the fluid moves along well defined parts or streamlines. In laminar flow all streamlines are straight and parallel. In laminar flow one layer of fluid is sliding over another layer, whenever the Reynolds number is less than 2000, the flow is said to be laminar. In laminar flow, energy loss is low and it is directly proportional to the velocity of the fluid. The following reasons are for the laminar flow, fluid has low velocity, fluid has high viscosity and diameter of pipe is large Turbulent Flow: The flow is said to be turbulent flow it he flow moves in a zigzag way. Due to movement of the particles in a zigzag way the eddies formation take place which are responsible of highenergy losses. 7-1

36 Reynolds s Apparatus In turbulent flow, energy loss is directly proportional to the square of velocity of fluid. If Reynolds number is greater than 4000, then flow is said to be turbulent Reynolds s Number Reynolds was first to determine the translation from laminar to turbulent depends not only on the mean velocity but on the quality Where, = Density of Fluid D = Diameter of pipe =Dynamic Viscosity Re = VD The term is dimensionless and it is called Reynolds Number (Re). It is the ration of the inertia force to the viscous force Re = Intertia Force Viscous Force Re = V2 ( V D ) Re = VD This indicates that it is non-dimensional number. Apparatus Description The apparatus consists of 1. A tank containing water at constant head 2. Die container 3. A glass tube 4. The water from the tank is allowed to flow through the glass tube. The velocity of flow can be varied by regulating valve. A liquid die having same specific weight as that of water has to be introduced to glass tube. Additional materials or Equipments required are 1. Stop Watch 2. Measuring Flask 3. Color Dye 4. Water Supply 7-2

37 Reynolds s Apparatus Experimental Procedure 1. Switch on the pump and fill the head tank. Manually also fill the dye tank with some amount of bright dye liquid provided. 2. Open the control valve slowly at the bottom of the tube and release small flow of dye. 3. Observe the flow in the tube. 4. Note down the time for 1 liter of discharge with the help of stopwatch and measuring flask. 5. Repeat the above process for various discharges Observations The following observations are made: 1. When the velocity of flow is low, the die filament in the glass tube is in the form of a straight line of die filament is parallel to the glass tube which is the case of laminar flow as shown in fig. Laminar flow 2. With the increase of velocity of flow the die filament is no longer straight line but it becomes wavy one as shown in fig. this is shown that flow is no longer laminar. This is transition flow. Transition flow 3. With further increase of velocity of the way die filament is broken and finally mixes in water as shown in fig. Turbulent flow 7-3

38 Reynolds s Apparatus Observation Table Sr. No. Time for 500 ml discharge in (Sec) Discharge Q (m 3 /s) Velocity V (m/s) Reynolds No. Re Observe the flow (Laminar, Transition, Turbulent) Conversion Factors 1 liter/sec = m 3 /sec 0.5 liter/sec = m 3 /sec Calculations Since D = 0.02 m Area = A = π 4 d2 = π 4 x = m 2 Ambient Temperature is 30 0 C, = x 10-6 Q = V = Q A = time required to collect 0.5 ltrs of water in m3 /sec Q in m/sec Re = VD = VD v (because ) Where, = Kinematic viscosity of water which in m 2 /s V = Velocity of Water in m/s D = Diameter of pipe is m Conclusion

39 Appendix Dynamic and Kinematic Viscosity of Water in SI Units:- Temperature t ( 0 C) Dynamic Viscosity µ (N.s/m 2 ) x 10-3 Reynolds s Apparatus Kinematic Viscosity ν (m 2 /s) x

40

41 EXPERIMENT NO. 8 Pipe Friction Losses Date: / / Objective To determine Fluid friction factor for the given pipes. Introduction The flow of liquid through a pipe is resisted by viscous shear stresses within the liquid and the turbulence that occurs along the internal walls of the pipe, created by the roughness of the pipe material. This resistance is usually known as pipe friction and is measured is meters head of the fluid, thus the term head loss is also used to express the resistance to flow. Many factors affect the head loss in pipes, the viscosity of the fluid being handled, the size of the pipes, the roughness of the internal surface of the pipes, the changes in elevations within the system and the length of travel of the fluid. The resistance through various valves and fittings will also contribute to the overall head loss. In a well designed system the resistance through valves and fittings will be of minor significance to the overall head loss and thus are called Major losses in fluid flow. The Darcy-Weisbach equation Weisbach first proposed the equation we now know as the Darcy-Weisbach formula or Darcy-Weisbach equation. Where, h f = Head loss in meter f = Darcy friction factor depends L = length of pipe work in meter V = Velocity of fluid in meter/sec D = inner diameter of pipe in meter h f = 4fLV2 2gD g = Acceleration due to gravity meter /second 2 The Darcy Friction factor used with Weisbach equation has now become the standard head loss equation for calculating head loss in pipes where the flow is turbulent. 8-1

42 Pipe Friction Losses Apparatus Description The experimental set up consists of a large number of pipes of different diameters. The pipes have tapping at certain distance so that a head loss can be measure with the help of a U Tube manometer. The flow of water through a pipeline is regulated by operating a control valve which is provided in main supply line. Actual discharge through pipeline is calculated by collecting the water in measuring tank and by noting the time for collection. Technical Specification Pipe: MOC = P.U. Test length = 1000 mm Pipe Dia. Pipe 1: ID: 16 mm Pipe 2: ID: 21 mm Pipe 3: ID: 26.5 mm Experimental Procedure 1. Fill the storage tank/sump with the water. 2. Switch on the pump and keep the control valve fully open and close the bypass valve to have maximum flow rate through the meter. 3. To find friction factor of pipe 1 open control valve of the same and close other to valves 4. Open the vent cocks provided for the particular pipe 1 of the manometer. 5. Note down the difference of level of mercury in the manometer limbs. 6. Keep the drain valve of the collection tank open till it s time to start collecting the water. 7. Close the drain valve of the collection tank and collect known quantity of water 8. Note down the time required for the same. 9. Change the flow rate of water through the meter with the help of control valve and repeat the above procedure. 10. Similarly for pipe 2 and 3. Repeat the same procedure indicated in step Take about 2-3 readings for different flow rates. 8-2

43 Pipe Friction Losses Observations Table Length of test section L = 1000 mm = 1 m Pipe 1 Internal Diameter of Pipe, D= 16 mm Cross Sectional Area of Pipe = mm 2 = 2.0 x 10-4 m 2 Sr. No. Qty (liters) t (sec) h 1 h 2 (mm) V (m/s) Pipe 2 Internal Diameter of Pipe, D= 21 mm Cross Sectional Area of Pipe = mm 2 = 3.46 x 10-4 m 2 Sr. No. Qty (liters) t (sec) h 1 h 2 (mm) V (m/s) Pipe 3 Internal Diameter of Pipe, D= 26.5 mm Cross Sectional Area of Pipe = mm 2 = 5.52 x 10-4 m 2 Sr. No. Qty (liters) t (sec) h 1 h 2 (mm) V (m/s)

44 Pipe Friction Losses Calculations 1. Q = L time required to collect L ltrs in m 3 /sec 2. Mean velocity, V = Q A in meter/sec According to Darcy- Weisbach Equation for frictional loss of head due to pipe friction h f = h 1 h 2 = 4fLV2 2gD In the above equation, everything is known to us except f Conversion Factor: 1 mm of Hg = m of water Conclusion

45 EXPERIMENT NO. 9 Objective To determine loss coefficients for different pipe fittings. DIFFERENT PIPE FITTINGS Date: / / Introduction While installing a pipeline for conveying a fluid, it is generally not possible to install a long pipeline of same size all over a straight for various reasons, like space restrictions, aesthetics, location of outlet etc. Hence, the pipe size varies and it also changes its direction. Also, various fittings are required to be used. All these variations of sizes and the fittings cause the loss of fluid head. Losses due to change in cross-section, bends, elbows, valves and fittings of all types fall into the category of minor losses in pipelines. In long pipeline, the friction losses are much larger than these minor losses and hence, the latter are often neglected. But, in shorter pipelines, their consideration is necessary for the correct estimate of losses. The minor loses are, generally expressed as Where, H L is the minor loss (i.e. head loss) H L = K L ( V2 2g ) K L, the loss coefficient, which is practically constant at high Reynolds s number for particular flow geometry V is the velocity of flow in the pipe (in case of sudden contraction, V is the velocity of flow in the contracted section). For an abrupt enlargement of the pipe section, however, use of the continuity equation, Bernoulli s equation and Momentum equation yields H L = (V V2 ) 2g H L = {1 ( d D ) 2 } V2 2g H L = K L ( V2 2g ) Here, V 2 = Velocity of flow in the larger diameter (= D) V = Velocity of flow in the smaller diameter (=d) 9-1

46 DIFFERENT PIPE FITTINGS Apparatus Description The experimental set-up consists of a pipe of diameter about 24.3 mm fitted with 1. A right angle bend 2. An elbow 3. A Gate Valve 4. A sudden expansion (larger pipe having diameter of about 24.3 mm) and 5. A sudden contraction (from about 24.3 mm to about 13.8 mm) Sufficient length of the pipeline is provided between various pipe fittings. The pressure taps on either side of these fittings are suitably provided and the same may be connected to a multi tube manometer bank. Supply to the line is made through a storage tank and discharge is regulated by means of outlet valve provided near the outlet end. Experimental Procedure 1. Fill up sufficient clean water in the sump tank 2. Fill up mercury in the manometer 3. Connect the electric supply. See that the flow control valve and bypass valve are fully open and all the manometer cocks are closed. Keep the water collecting funnel in the sump tank side 4. Start the pump and adjust the flow rate. Now slowly open the manometer tapping connection of small bend. Open both the cocks simultaneously 5. Open air vent cocks. Remove air bubbles and slowly & simultaneously close the cocks. Note down the manometer reading and flow rate. 6. Close the cocks and similarly, note down the readings for other fittings. Repeat the procedure for different flow rates. Observations: Type of fitting Elbow Sr. No. Manometer diff. mm of Hg Flow rate (Time for L liters of water) t sec

47 5 DIFFERENT PIPE FITTINGS Type of fitting Bend Sr. No. Manometer diff. mm of Hg Flow rate (Time for L liters of water) t sec Type of fitting Valve Sr. No. Manometer diff. mm of Hg Flow rate (Time for L liters of water) t sec Type of fitting Sudden Contraction Sr. No. Manometer diff. mm of Hg Flow rate (Time for L liters of water) t sec Type of fitting Sudden Expansion Sr. No. Manometer diff. mm of Hg Flow rate (Time for L liters of water) t sec

48 DIFFERENT PIPE FITTINGS Calculations 1. Elbow In elbow, there is no change in the magnitude of velocity of water but there is change in the direction of water, hence head loss exists Diameter of the elbow, d = 33.4 mm = m For elbow, mean area A = π 4 d2 = 8.76 x 10 4 m 2 Where, Q = Therefore, loss of head at elbow Mean velocity of flow, V = Q A m/s L time required to collect L ltrs of water in m3 /sec H L = K L ( V2 ) meter of water 2g Where, H L = Manometer difference (m) Pipe Bend Similar to elbow, loss of head at bend is due to change in the direction of water. But unlike the elbow, change of direction is not abrupt hence loss if head is les compared to elbow Diameter of the bend, d = 33.4 mm = m For bend, mean area A = π 4 d2 = 8.76 x 10 4 m 2 Where, Q = Therefore, loss of head at bend Mean velocity of flow, V = Q A m/s L time required to collect L ltrs of water in m3 /sec H L = K L ( V2 ) meter of water 2g Where, H L = Manometer difference (m)

49 DIFFERENT PIPE FITTINGS 3. Valve Diameter of the valve opening, d = 33.4 mm = m For gate valve, mean area A = π 4 d2 = 8.76 x 10 4 m 2 Where, Q = Therefore, loss of head at bend Mean velocity of flow, V = Q A m/s L time required to collect L ltrs of water in m3 /sec H L = K L ( V2 ) meter of water 2g Where, H L = Manometer difference (m) Sudden Contraction At sudden contraction, velocity of water increases which causes pressure head to drop (according to Bernoulli s Theorem) in addition to this there is loss of head due to sudden contraction. Hence, Manometer reading = (Head drop due to increment of velocity) + (head loss due to sudden contraction) Assuming no loss to be there due to contraction and applying Bernoulli s theorem at inlet and outlet of the section 2 P i w + v i 2g = P o w + v 2 o 2g Inlet size (dia.) = 24.3 mm = m; Therefore A i = 4.64 X 10-4 m 2 Outlet size (dia.) = 13.8 mm = m; Therefore A o = 1.50 x 10-4 m 2 Where, Q = V i = Q m s and V A o = Q m s i A o A i and A o = inlet and outlet area respectively in m 2 Drop of Head due to velocity increment, L time required to collect L ltrs of water in m3 /sec h v = v i 2 2g v 2 o 2g 9-5

50 DIFFERENT PIPE FITTINGS Actual drop, h = (manometer reading x 12.6) Loss of head due to sudden contraction, H LC = h h v Thepritically, h Lc = K L ( V o 2 2g ) 5. Sudden Expansion At sudden expansion of flow, pressure increases due to reduction in velocity, but there is pressure drop due to sudden expansion also. Hence at sudden expansion one rise of pressure lesser than that predicated theoretically. Assuming no loss of head and applying Bernoulli s equation at inlet and outlet, similar to equation used for sudden contraction, Actual drop, h = (manometer reading x 12.6) Rise of pressure h v = v i 2 2g v 2 o 2g Loss of head due to sudden expansion, H Le = h v h Thepritically, h Le = K L (V i V o ) 2 2g Result Table Sr No Bend Elbow Valve Sudden Contraction Sudden Expansion h L K L h L K L h L K L h Lc K L h Le K L Conclusion

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