Chapter 5: Mass, Bernoulli and Energy Equations

1. PTT 204/3APPLIED FLUID MECHANICSSEM 2 (2012/2013) Chapter 5: Mass, Bernoulli and Energy Equations

2. Objectives • Apply the conservation of mass equation to balance the incoming and outgoing flow rates in a flow system. • Recognize various forms of mechanical energy, and work with energy conversion efficiencies. • Understand the use and limitations of the Bernoulli equation, and apply it to solve a variety of fluid flow problems. • Work with the energy equation expressed in terms of heads, and use it to determine turbine power output and pumping power requirements.

3. 5–1 ■ INTRODUCTION You are already familiar with numerous conservation lawssuch as the lawsof conservation of mass, conservation of energy, and conservation ofmomentum. Historically, the conservation laws are first applied to a fixedquantity of matter called a closed systemor just a system, and then extendedto regions in space called control volumes. The conservation relations arealso called balance equationssince any conserved quantity must balanceduring a process.

4. the total rates of mass flow into and out of the controlvolume the rate of change of mass withinthe control volume boundaries. Conservation of Mass The conservation of mass relation for a closed system undergoing a changeis expressed as msys = constant or dmsys/dt = 0, which is the statement thatthe mass of the system remains constant during a process. Mass balance for a control volume(CV)in rate form: Continuityequation: In fluid mechanics, the conservation of massrelation written for a differential control volume is usually called the continuityequation.

5. The Linear Momentum Equation Linearmomentum:The product of the mass and the velocity of a body is called the linearmomentum or just the momentum of the body. The momentum of a rigidbody of mass mmoving with a velocity Vis m . Newton’s second law:The acceleration of a body is proportional to the net force acting on itand is inversely proportional to its mass, and that the rate of change of themomentum of a body is equal to the net force acting on the body. Conservation of momentum principle:The momentum of a system remains constant only when the net force actingon it is zero, and thus the momentum of such systems is conserved. Linear momentum equation:In fluid mechanics, Newton’ssecond law is usually referred to as the linear momentum equation.

6. Conservation of Energy The conservation of energy principle (the energy balance):The net energy transfer toor from a system during a process be equal to the change in the energy contentof the system. Energy can be transferred to or from a closed system by heat or work. Control volumes also involve energy transfer via mass flow. the total rates of energy transfer into and out of thecontrol volume the rate of change of energy within the control volume boundaries In fluid mechanics, we usually limitour consideration to mechanical forms of energy only.

7. 5–2 ■MECHANICAL ENERGY AND EFFICIENCY Mechanical energy:The form of energy that can be converted to mechanical work completely and directly by an ideal mechanical device such as an ideal turbine. Mechanical energy of a flowing fluid per unit mass: Flow energy + kinetic energy + potential energy Mechanical energy change: • The mechanical energy of a fluid does not change during flow ifits pressure, density, velocity, and elevation remain constant. • In the absenceof any irreversible losses, the mechanical energy change represents the mechanicalwork supplied to the fluid (if emech > 0) orextracted from thefluid (if emech < 0).

8. Mechanical energy is illustrated byan ideal hydraulic turbine coupledwith an ideal generator. In the absenceof irreversible losses, the maximumproduced power is proportional to(a) the change in water surfaceelevation from the upstream to thedownstream reservoir or (b) (close-upview) the drop in water pressure fromjust upstream to just downstream ofthe turbine.

9. Shaft work:The transfer of mechanical energy is usually accomplished by a rotatingshaft, and thus mechanical work is often referred to as shaft work. A pumpor a fan receives shaft work (usually from an electric motor) and transfers itto the fluid as mechanical energy (less frictional losses). A turbine converts the mechanical energy of a fluid to shaft work. Mechanicalefficiencyof a device or process The effectiveness of the conversion process between the mechanical work supplied or extracted and the mechanical energy of the fluid is expressed by the pump efficiencyand turbine efficiency,

10. The mechanical efficiency of a fanis the ratio of the rate of increase ofthe mechanical energy of the air to themechanical power input.

11. Motor efficiency Generator efficiency Pump-Motor overall efficiency Turbine-Generator overall efficiency: The overall efficiency of a turbine–generator is the product of the efficiency of the turbine and the efficiency of the generator, and represents the fraction of the mechanical energy of the fluid converted to electric energy.

12. The efficiencies just defined range between 0 and 100%. 0% corresponds to the conversion of the entiremechanical or electric energy input to thermal energy, and the device inthis case functions like a resistance heater. 100%corresponds to the case of perfect conversion with no friction or other irreversibilities,and thus no conversion of mechanical or electric energy tothermal energy (no losses). For systems that involve only mechanicalforms of energy and its transfer as shaft work, the conservation of energy is Emech, loss: The conversion of mechanical energy to thermalenergy due toirreversibilities such as friction. Many fluid flow problems involvemechanical forms of energy only, andsuch problems are conveniently solvedby using a mechanical energy balance.

15. 5–3 ■THE BERNOULLI EQUATION Bernoulli equation:An approximate relation between pressure,velocity, and elevation, and is valid in regions of steady, incompressibleflow where net frictional forces are negligible. Despite itssimplicity, it has proven to be a very powerful tool in fluid mechanics. The Bernoulliapproximation is typically useful in flow regions outside of boundary layersand wakes, where the fluid motion isgoverned by the combined effects ofpressure and gravity forces. The Bernoulli equation is anapproximate equation that is validonly in inviscid regions of flow wherenet viscous forces are negligibly smallcompared to inertial, gravitational, orpressure forces. Such regions occuroutside of boundary layers and wakes.

16. Acceleration of a Fluid Particle In two-dimensional flow,the acceleration can be decomposed into two components: streamwiseacceleration asalong the streamline and normal acceleration anin thedirection normal to the streamline, which is given asan =V2/R. Streamwise acceleration is due to a change in speed along a streamline, andnormal acceleration is due to a change in direction. For particles that movealong a straight path, an= 0 since the radius of curvature is infinity andthus there is no change in direction. The Bernoulli equation results from aforce balance along a streamline. During steady flow, a fluid may notaccelerate in time at a fixed point, butit may accelerate in space. Acceleration in steady flow is due to the change ofvelocity with position.

17. Derivation of the Bernoulli Equation Bernoulli equation Steady flow: Steady, incompressible flow: The forces acting on a fluid particlealong a streamline. The sum of the kinetic, potential, and flowenergies of a fluid particleis constant along a streamline during steady flow whencompressibilityand frictional effects are negligible. The Bernoulli equation between any two points on thesame streamline:

18. The incompressible Bernoulliequation is derived assumingincompressible flow, and thus itshould not be usedfor flows with significantcompressibility effects.

19. Unsteady, Compressible Flow The Bernoulli equation for unsteady, compressible flow:

20. The Bernoulli equation can beviewed as the“conservation of mechanical energy principle.” • This is equivalentto the general conservation ofenergy principle for systems that do notinvolve any conversion of mechanical energy and thermal energy to eachother, and thus the mechanical energy and thermal energy are conserved separately. • The Bernoulli equation states that during steady, incompressible flowwith negligible friction, the various forms of mechanical energy are convertedto each other, but their sum remains constant. • There isno dissipation ofmechanical energy during such flows since there is no frictionthat converts mechanical energy to sensible thermal (internal) energy. • TheBernoulli equation is commonly used in practice since a variety of practicalfluid flow problems can be analyzed to reasonable accuracy with it. The Bernoulli equation states that thesum of the kinetic, potential, and flowenergies of a fluid particle is constantalong a streamline during steady flow.

21. Static, Dynamic, and Stagnation Pressures Thekinetic and potential energies of the fluid can be converted to flow energy(and vice versa) during flow, causing the pressure to change.Multiplying the Bernoulli equation by thedensity gives P is the static pressure:It does not incorporate any dynamic effects; itrepresents the actual thermodynamic pressure of the fluid. This is thesame as the pressure used in thermodynamics and property tables. V2/2 is the dynamic pressure:It represents the pressure rise when thefluid in motion is brought to a stop isentropically. gz is the hydrostatic pressure:It is not pressure in a real sensesince its value depends on the reference level selected; it accounts for theelevation effects, i.e., fluid weight on pressure. (Be careful of the sign—unlikehydrostatic pressure gh which increases with fluid depth h, thehydrostatic pressure term gz decreases with fluid depth.) Totalpressure:The sum of the static, dynamic, and hydrostatic pressures. Therefore, the Bernoulli equation states that the total pressurealong a streamline is constant.

22. Stagnationpressure: The sum of the static and dynamicpressures. It represents the pressure at a point where the fluid isbrought to a complete stop isentropically. Close-up of a Pitot-static probe,showing the stagnation pressurehole and two of the five staticcircumferential pressure holes. The static,dynamic, andstagnationpressuresmeasured usingpiezometer tubes.

23. When a stationary body is immersed in a flowing stream, the fluid is brought to a stop at the nose of the body (stagnation point) Stagnation point Streaklines produced by colored fluidintroduced upstream of an airfoil;since the flow is steady, the streaklinesare the same as streamlines andpathlines. The stagnation streamlineis marked.

24. Limitations on the Use of the Bernoulli Equation • Steady flowThe Bernoulli equation is applicable to steady flow. • Frictionless flowEvery flow involves some friction, no matter how small, and frictional effects may or may not be negligible. • No shaft workThe Bernoulli equation is not applicable in a flow section that involves a pump, turbine, fan, or any other machine or impeller since such devices destroy the streamlines and carry out energy interactions with the fluid particles. When these devices exist, the energy equation should be used instead. • Incompressible flowDensity is taken constant in the derivation of the Bernoulli equation. The flow is incompressible for liquids and also by gases at Mach numbers less than about 0.3. • No heat transferThe density of a gas is inversely proportional to temperature, and thus the Bernoulli equation should not be used for flow sections that involve significant temperature change such as heating or cooling sections. • Flow along a streamlineStrictly speaking, the Bernoulli equationis applicable along a streamline. However, when a region of the flow is irrotational and there is negligibly small vorticity in the flow field, the Bernoulli equation becomes applicable across streamlines as well.

25. Frictional effects, heat transfer, and components thatdisturb the streamlined structure offlow make theBernoulli equation invalid. It shouldnot be used in any of the flows shownhere. When the flow is irrotational, theBernoulli equation becomes applicablebetween any two points along the flow(not just on the same streamline).

26. Hydraulic Grade Line (HGL)and Energy Grade Line (EGL) It is often convenient to represent the level of mechanical energy graphicallyusing heightsto facilitate visualization of the various terms of the Bernoulliequation. Dividing each term of the Bernoulli equation by ggives P/g is the pressure head; it represents the height of a fluid column thatproduces the static pressure P. V2/2g is the velocity head; it represents the elevation needed for a fluidto reach the velocity V during frictionless free fall. z is the elevation head; it represents the potential energy of the fluid. An alternative form of the Bernoulliequation is expressed in terms ofheads as: The sum of the pressure,velocity, and elevation heads isconstant along a streamline.

27. Hydraulic grade line (HGL), P/g + zThe line that represents the sum of the static pressure and the elevationheads. Energygrade line (EGL), P/g + V2/2g + zThe line thatrepresentsthe total head of the fluid. Dynamic head,V2/2gThe difference between the heights of EGL and HGL. The hydraulic grade line (HGL) andthe energy grade line (EGL) for freedischarge from a reservoir through ahorizontal pipe with a diffuser.

28. Noteson HGL and EGL • For stationary bodiessuch as reservoirs or lakes, the EGL and HGLcoincide with the free surface of the liquid. • The EGL is always a distance V2/2g above the HGL. These two curvesapproach each other as the velocity decreases, and they diverge as thevelocity increases. • In an idealized Bernoulli-type flow, EGL is horizontal and its heightremains constant. • For open-channel flow, the HGL coincides with the free surface of theliquid, and the EGL is a distance V2/2g above the free surface. • At a pipe exit, the pressure head is zero (atmospheric pressure) and thusthe HGL coincides with the pipe outlet. • The mechanical energy lossdue to frictional effects (conversion tothermal energy) causes the EGL and HGL to slope downward in thedirection of flow. The slope is a measure of the head loss in the pipe. Acomponent, such as a valve, that generates significant frictional effectscauses a sudden drop in both EGL and HGL at that location. • A steep jump/dropoccurs in EGL and HGL whenever mechanical energy is added/removed to/from the fluid (pump/turbine). • The (gage) pressure of a fluid is zero at locations where the HGLintersects the fluid. The pressure in a flow section that lies above the HGLis negative, and the pressure in a section that lies below the HGL ispositive.

29. In an idealized Bernoulli-type flow,EGL is horizontal and its heightremains constant. But this is notthe case for HGL when the flowvelocity varies along the flow. A steep jump occurs in EGL and HGLwhenever mechanical energy is addedto the fluid by a pump, and a steep dropoccurs whenever mechanical energy isremoved from the fluid by a turbine. The gage pressure of a fluid is zeroat locations where the HGL intersectsthe fluid, and the pressure is negative(vacuum) in a flow section that liesabove the HGL.

30. Example: Water Discharge from a Large Tank Example: Spraying Water into the Air

31. Example: Siphoning Out Gasoline from a Fuel Tank

32. Example: Velocity Measurement by a Pitot Tube

33. Example: The Rise of the Ocean Due to a Hurricane The eye of hurricane Linda (1997in the Pacific Ocean near BajaCalifornia) is clearly visible inthis satellite photo.

37. 5–5 ■GENERAL ENERGY EQUATION The first law of thermodynamics (the conservation of energy principle): Energy cannot be created ordestroyed during a process;it can only change forms. The energy change of a systemduring a process is equal to the network and heat transfer between thesystem and its surroundings.

38. Energy Transfer by Heat, Q Thermal energy: The sensible and latent forms of internal energy. Heat Transfer:The transfer of energy from one system to another as a result of a temperature difference. The direction of heat transfer is always from the higher-temperature body to the lower-temperature one. Adiabatic process:A process during which there is no heat transfer. Heat transfer rate:The time rate of heat transfer. Temperature difference is the driving force for heat transfer. The larger the temperature difference, the higher is the rate of heat transfer.

39. Energy Transfer by Work, W • Work:The energy transfer associated with a force acting through a distance. • A rising piston, a rotating shaft,andan electric wire crossing the system boundaries are all associated with work interactions. • Power: The time rate ofdoing work. • Car engines and hydraulic,steam, and gas turbines produce work; compressors, pumps, fans, and mixersconsume work. WshaftThe work transmitted by a rotating shaft WpressureThe workdone by the pressure forces on the control surface WviscousThe work doneby the normal and shear components of viscous forces on the control surface WotherThe work done by other forces such as electric, magnetic,and surface tension

40. Shaft Work A force F acting through a moment arm r generates a torque T This force acts through a distance s Shaft work The power transmitted through the shaft is the shaft work done per unit time: Shaft work is proportional to the torque applied and the number of revolutions of the shaft. Energy transmission through rotating shafts is commonly encountered in practice.

41. Work Done by Pressure Forces The pressure force acting on (a) themoving boundary of a system ina piston-cylinder device, and(b) the differential surface areaof a system of arbitraryshape.

42. The conservation of energy equationis obtained by replacing B in theReynolds transport theorem byenergy E and b by e.

43. In a typical engineering problem, thecontrol volume may contain manyinlets and outlets; energy flows in ateach inlet, and energy flows out ateach outlet. Energy also enters thecontrol volume through net heattransfer and net shaft work.

44. 5–6 ■ENERGY ANALYSIS OF STEADY FLOWS The net rate of energy transfer to a control volume by heattransfer and work during steady flow is equal to the difference between therates of outgoing and incoming energy flows bymass flow. single-stream devices A control volume with only one inletand one outlet and energy interactions.

45. Ideal flow (no mechanical energy loss): The lost mechanical energy in a fluidflow system results in an increase inthe internal energy of the fluid andthus in a rise of fluid temperature. Real flow (with mechanical energy loss):

46. A typical power plant has numerouspipes, elbows, valves, pumps, andturbines, all ofwhich have irreversiblelosses.

47. Energy equationin terms ofheads

48. Mechanical energy flow chart fora fluid flow system that involvesa pump and a turbine. Verticaldimensions show each energyterm expressed as anequivalentcolumn height of fluid, i.e., head.

49. (5-74) Special Case: Incompressible Flow with No Mechanical Work Devices and Negligible Friction When piping losses are negligible, there is negligible dissipation of mechanicalenergy into thermal energy, and thus hL=emech loss, piping /g ≅ 0. Also, hpump, u=hturbine, e= 0 when there are nomechanical work devices such as fans, pumps, or turbines. Then Eq. 5–74reduces to This is the Bernoulli equationderived earlier using Newton’s second lawof motion. Thus, the Bernoulli equation can be thought of as a degenerateform of the energy equation.

50. Kinetic Energy Correction Factor,  The kinetic energy of a fluid stream obtained from V2/2 is not the same as theactual kinetic energy of the fluid stream since the square of a sum is not equalto the sum of the squares of its components. This error can becorrected by replacing the kinetic energy terms V2/2 in the energy equation byVavg2/2, where  is the kinetic energy correctionfactor. Thecorrection factor is 2.0 for fully developed laminarpipe flow, and it rangesbetween 1.04 and 1.11 for fully developed turbulent flow in a round pipe. The determination of the kineticenergy correction factor using theactual velocity distribution V(r) andthe average velocity Vavg at a crosssection.