Two Phase Flows (Section 3) The Basic Model

Size: px
Start display at page:

Download "Two Phase Flows (Section 3) The Basic Model"

Transcription

1 Two Phase Flows (Section 3) By: Pro. M. H. Saidi Center o Excellence in Energy Conversion Shari University o Technology

2 Homewor Homewor set#1 Problems 1,,3,4; Chapter 1, Collier and Thome. Due to next Tuesday (Mehr, 14th)

3 Time Averaging B 1 T = T 0 Bdt

4 Volume Averaging Bˆ 1 = V V BdV Volume Averaging { B} 1 = V c V c BdV Phase Averaging Relation between phase and volume averaging or continues phase { B} = α Bˆ c

5 Principal Equation o Two Phase Flow 1. One dimensional low. Steady state 3. Constant physical properties 4. Existence o Thermodynamic equilibrium

6 Conservation o Mass α ρ t Z ( Aα ρ ) + ( Aα ρu ) = Γ Void raction o phase Density o phase Continuity equation o phase For steady state low Γ Mass Generation rate per Γ = 0 unit length or phase t ( Aα ρ ) = 0 For gas (g)- liquid () two phase low d ( A ρ u ) =Γ d ( ρ u ) =Γ g g g g dw g Γ g = Γ = = dw

7 Conservation o Momentum t ( W δz) + ( W u + δz ( W u )) W u z t ( W δz) + δz ( W u ) z rate o creation o momentum o phase rate o inlow o momentum within the control volume W = Aα ρ u Pressure orces on the element Aα p Aα p + δz ( Aα p) p δz ( Aα ) z z Aα ρδzg sinθ τ ρδzg sinθ τ P δz + τ P δz + u Γ w w w nz n 1 Gravity Wall shear Interacial shear n Rate o momentum generation

8 Conservation o Momentum Force= creation o momentum + inlow o momentum within the control volume n p Aα δz τ P δz + τ P δz Aα ρδzg sinθ + u Γ w w nz n z 1 = ( W δz) + δz ( W u ) t z Steady gas- liquid two phase low Adp τ P + τ P A ρ g sinθ + u Γ = W du g gw gw g g g g g g g g Adp τ P + τ P A ρ g sinθ + u Γ = W du w w g g Ι И Momentum conservation at interace τ P + u Γ = τ P + u Γ g g g g g g Ш

9 Conservation o Momentum summation o equation Ι, И & Ш * Adp τ P τ P g sin θ( A ρ + A ρ ) = dw ( u + W u ) gw gw w w g g g g Friction orce or each phase ** dp ( dfg + S) = τgwpgw τg Pg = Ag( gf ) dp ( df S) = τwpw + τg Pg = A ( F ) dp ( dfg + df ) = τgwpgw τwpw = A( F ) Part o total pressure gradient which is need or prevalence o riction

10 Conservation o Momentum substitution equation ** in * yields ( dp ) = ( dp F) + ( dp a) + ( dp z) dp 1 d d x ν g (1 x) ν ( a) = ( W gug + W u ) = G + A α (1 α) dp Ag A ( z ) = g sinθ ρg ρ g sin θ αρg (1 α) ρ + = + A A Total pressure lost

11 Energy Conservation t u u u u [ αρ ( ε + ) Aδz] + W ( ε + ) δz [ W ( ε + ) δz W ( ε + )] z A rate o increase o total energy in the C.V rate o entrance o energy within the control volume ε Internal energy per unit mass Rate o heat entrance to C.V o phase n φ P δz + φ P δz + φ& Aαδz w w n n 1 B Heat low rom channel wall H.V. via the various interaces Internal heat generation within C.V

12 Energy Conservation The wor done by pressure orces Wor done by expansion o phase W p W p W p α δz ( ) W g sinθδz paδz ρ + ρ z ρ t n δzp +Γ + u τ P δ z n n ρ 1 The wor done by body orce C Wor done by pressure and shear orces at the interace with the other phases Mass generation rate per unit length u Γ δz ( ε + ) D

13 A=B+C+D Enthalpy o phase Energy Conservation u u Aα ρ ε W i W g θ φ P t z α u + + +Γ + + ( + ) + ( + ) = sin + w w n n φnpn φ& Aα pa ( i ) u τnpn 1 t 1 i = u + p ρ For steady gas- liquid two phase low in channel with constant area u g d W g( ig + ) + W g g sinθδz = u φwgpwgδz + φg Pgδz + ugτg Pgδz +Γ gδz( ig + ) u d W ( i + ) + W g sinθδz = u φw Pwδz + φgpgδz + uτgpgδz +Γ δz ( i + )

14 Energy Conservation Energy conservation at interace ug u φg Pg + ugτg Pgδz +Γ g( ig + ) = φw Pwδz + φgpgδz + uτgpgδz +Γ δz( i + ) with regard the equations, and d W u [ W i W i ] [ ] ( W W ) g sin Q d g g W u g g g + θ = w1 Heat transer to the luid across the channel wall per unit length Q ( = φ p + φ p ) wl w w wg wg

15 Energy Conservation Total pressure gradient Frictional dissipation dp de Q [ xνg + (1 x) ν ] = W 3 3 d G d xv g (1 x) v + p [ xνg + (1 x) ν ] + + g sinθ + α (1 α) w Acceleration head term Static head term Internal energy per unit mass E = xε + (1 x) ε g

16 Use o the momentum or energy equation to evaluate the pressure gradient Using momentum equation Using void raction to calculate acceleration term rom dp 1 d d x ν g (1 x) ν ( a) = ( W gug + W u ) = G + A α (1 α) or static head term rom dp Ag A ( z ) = g sinθ ρg + ρ = g sin θ αρg + (1 α) ρ A A Then calculating riction pressure term rom correlation equation in terms o independent variables.

17 Use o the momentum or energy equation to evaluate the pressure gradient Using energy equation Calculation o pressure lost arising rom variation o potential energy Calculation o pressure lost arising rom variation o inetic energy Calculate the riction pressure term rom independent variables Note: in two methods we need to the void raction but the degree o importance in each method is not the same.

OE4625 Dredge Pumps and Slurry Transport. Vaclav Matousek October 13, 2004

OE4625 Dredge Pumps and Slurry Transport. Vaclav Matousek October 13, 2004 OE465 Vaclav Matousek October 13, 004 1 Dredge Vermelding Pumps onderdeel and Slurry organisatie Transport OE465 Vaclav Matousek October 13, 004 Dredge Vermelding Pumps onderdeel and Slurry organisatie

More information

1 Introduction to Governing Equations 2 1a Methodology... 2

1 Introduction to Governing Equations 2 1a Methodology... 2 Contents 1 Introduction to Governing Equations 2 1a Methodology............................ 2 2 Equation of State 2 2a Mean and Turbulent Parts...................... 3 2b Reynolds Averaging.........................

More information

Analysis of Non-Thermal Equilibrium in Porous Media

Analysis of Non-Thermal Equilibrium in Porous Media Analysis o Non-Thermal Equilibrium in Porous Media A. Nouri-Borujerdi, M. Nazari 1 School o Mechanical Engineering, Shari University o Technology P.O Box 11365-9567, Tehran, Iran E-mail: anouri@shari.edu

More information

FLOW CHARACTERISTICS OF HFC-134a IN AN ADIABATIC HELICAL CAPILLARY TUBE

FLOW CHARACTERISTICS OF HFC-134a IN AN ADIABATIC HELICAL CAPILLARY TUBE E HEFAT7 5 th International Conerence on Heat Transer, Fluid Mechanics and Thermodynamics Sun City, South Arica Paper number: KM1 FLOW CHARACTERISTICS OF HFC-1a IN AN ADIABATIC HELICAL CAPILLARY TUBE Khan

More information

39.1 Gradually Varied Unsteady Flow

39.1 Gradually Varied Unsteady Flow 39.1 Gradually Varied Unsteady Flow Gradually varied unsteady low occurs when the low variables such as the low depth and velocity do not change rapidly in time and space. Such lows are very common in

More information

2/28/2006 Statics ( F.Robilliard) 1

2/28/2006 Statics ( F.Robilliard) 1 2/28/2006 Statics (.Robilliard) 1 Extended Bodies: In our discussion so far, we have considered essentially only point masses, under the action of forces. We now broaden our considerations to extended

More information

Fluid Mechanics II Viscosity and shear stresses

Fluid Mechanics II Viscosity and shear stresses Fluid Mechanics II Viscosity and shear stresses Shear stresses in a Newtonian fluid A fluid at rest can not resist shearing forces. Under the action of such forces it deforms continuously, however small

More information

2, where dp is the constant, R is the radius of

2, where dp is the constant, R is the radius of Dynamics of Viscous Flows (Lectures 8 to ) Q. Choose the correct answer (i) The average velocity of a one-dimensional incompressible fully developed viscous flow between two fixed parallel plates is m/s.

More information

FLUID MECHANICS PROF. DR. METİN GÜNER COMPILER

FLUID MECHANICS PROF. DR. METİN GÜNER COMPILER FLUID MECHANICS PROF. DR. METİN GÜNER COMPILER ANKARA UNIVERSITY FACULTY OF AGRICULTURE DEPARTMENT OF AGRICULTURAL MACHINERY AND TECHNOLOGIES ENGINEERING 1 5. FLOW IN PIPES 5.1.3. Pressure and Shear Stress

More information

PIPE FLOWS: LECTURE /04/2017. Yesterday, for the example problem Δp = f(v, ρ, μ, L, D) We came up with the non dimensional relation

PIPE FLOWS: LECTURE /04/2017. Yesterday, for the example problem Δp = f(v, ρ, μ, L, D) We came up with the non dimensional relation /04/07 ECTURE 4 PIPE FOWS: Yesterday, for the example problem Δp = f(v, ρ, μ,, ) We came up with the non dimensional relation f (, ) 3 V or, p f(, ) You can plot π versus π with π 3 as a parameter. Or,

More information

BERNOULLI EQUATION. The motion of a fluid is usually extremely complex.

BERNOULLI EQUATION. The motion of a fluid is usually extremely complex. BERNOULLI EQUATION The motion of a fluid is usually extremely complex. The study of a fluid at rest, or in relative equilibrium, was simplified by the absence of shear stress, but when a fluid flows over

More information

DEVELOPED LAMINAR FLOW IN PIPE USING COMPUTATIONAL FLUID DYNAMICS M.

DEVELOPED LAMINAR FLOW IN PIPE USING COMPUTATIONAL FLUID DYNAMICS M. DEVELOPED LAMINAR FLOW IN PIPE USING COMPUTATIONAL FLUID DYNAMICS M. Sahu 1, Kishanjit Kumar Khatua and Kanhu Charan Patra 3, T. Naik 4 1, &3 Department of Civil Engineering, National Institute of technology,

More information

Models of ocean circulation are all based on the equations of motion.

Models of ocean circulation are all based on the equations of motion. Equations of motion Models of ocean circulation are all based on the equations of motion. Only in simple cases the equations of motion can be solved analytically, usually they must be solved numerically.

More information

Numerical Heat and Mass Transfer

Numerical Heat and Mass Transfer Master Degree in Mechanical Engineering Numerical Heat and Mass Transfer 15-Convective Heat Transfer Fausto Arpino f.arpino@unicas.it Introduction In conduction problems the convection entered the analysis

More information

FLUID FLOW. Note that the balance is per unit mass. In differential form:

FLUID FLOW. Note that the balance is per unit mass. In differential form: Mechanical Energy Balance FLUI FLOW gδz ρ V Δ Wo F potential expansion ketic work added/ sum o energy work energy change subtracted by riction change pumps or losses compressors Note that the balance is

More information

FLUID MECHANICS. Lecture 7 Exact solutions

FLUID MECHANICS. Lecture 7 Exact solutions FLID MECHANICS Lecture 7 Eact solutions 1 Scope o Lecture To present solutions or a ew representative laminar boundary layers where the boundary conditions enable eact analytical solutions to be obtained.

More information

= v 0 x. / t = 1.75m / s 2.25s = 0.778m / s 2 nd law taking left as positive. net. F x ! F

= v 0 x. / t = 1.75m / s 2.25s = 0.778m / s 2 nd law taking left as positive. net. F x ! F Multiple choice Problem 1 A 5.-N bos sliding on a rough horizontal floor, and the only horizontal force acting on it is friction. You observe that at one instant the bos sliding to the right at 1.75 m/s

More information

6. Laminar and turbulent boundary layers

6. Laminar and turbulent boundary layers 6. Laminar and turbulent boundary layers John Richard Thome 8 avril 2008 John Richard Thome (LTCM - SGM - EPFL) Heat transfer - Convection 8 avril 2008 1 / 34 6.1 Some introductory ideas Figure 6.1 A boundary

More information

V (r,t) = i ˆ u( x, y,z,t) + ˆ j v( x, y,z,t) + k ˆ w( x, y, z,t)

V (r,t) = i ˆ u( x, y,z,t) + ˆ j v( x, y,z,t) + k ˆ w( x, y, z,t) IV. DIFFERENTIAL RELATIONS FOR A FLUID PARTICLE This chapter presents the development and application of the basic differential equations of fluid motion. Simplifications in the general equations and common

More information

Two Phase Flows (Section 7) Empirical Treatments of Two Phase Flow

Two Phase Flows (Section 7) Empirical Treatments of Two Phase Flow Two Phase Flows (Section 7 Empirical Treatments o Two Phase Flow By: Pro. M. H. Saidi enter o Excellence in Enery onversion School o Mechanical Enineerin Shari University o Technoloy Drit Flx Model Zber

More information

Numerical investigation of multiple slot jets in air knife coating

Numerical investigation of multiple slot jets in air knife coating Numerical investigation of multiple slot jets in air knife coating A. Yahyaee Soufiani 1, J.R. McDermid 2, A.N. Hrymak 3 and F.E. Goodwin 4 1 McMaster University 128 Main street west, Hamilton, ON, Canada,

More information

Lesson 6 Review of fundamentals: Fluid flow

Lesson 6 Review of fundamentals: Fluid flow Lesson 6 Review of fundamentals: Fluid flow The specific objective of this lesson is to conduct a brief review of the fundamentals of fluid flow and present: A general equation for conservation of mass

More information

Differential relations for fluid flow

Differential relations for fluid flow Differential relations for fluid flow In this approach, we apply basic conservation laws to an infinitesimally small control volume. The differential approach provides point by point details of a flow

More information

Steven Burian Civil & Environmental Engineering September 25, 2013

Steven Burian Civil & Environmental Engineering September 25, 2013 Fundamentals of Engineering (FE) Exam Mechanics Steven Burian Civil & Environmental Engineering September 25, 2013 s and FE Morning ( Mechanics) A. Flow measurement 7% of FE Morning B. properties Session

More information

Summary of Dimensionless Numbers of Fluid Mechanics and Heat Transfer

Summary of Dimensionless Numbers of Fluid Mechanics and Heat Transfer 1. Nusselt number Summary of Dimensionless Numbers of Fluid Mechanics and Heat Transfer Average Nusselt number: convective heat transfer Nu L = conductive heat transfer = hl where L is the characteristic

More information

CHARACTERISTIC OF FLUIDS. A fluid is defined as a substance that deforms continuously when acted on by a shearing stress at any magnitude.

CHARACTERISTIC OF FLUIDS. A fluid is defined as a substance that deforms continuously when acted on by a shearing stress at any magnitude. CHARACTERISTIC OF FLUIDS A fluid is defined as a substance that deforms continuously when acted on by a shearing stress at any magnitude. In a fluid at rest, normal stress is called pressure. 1 Dimensions,

More information

Fluid mechanics (wb1225)

Fluid mechanics (wb1225) Fluid mechanics (wb225) Lecture 8: flows through pipes and ducts Examples of pipe flows [] [2] [3] [4] 2 Flow states in pipe flow [5] Re crit 2300 3 Laminar vs turbulent [5] [6] 4 Pipe flow transition

More information

Transport Properties: Momentum Transport, Viscosity

Transport Properties: Momentum Transport, Viscosity Transport Properties: Momentum Transport, Viscosity 13th February 2011 1 Introduction Much as mass(material) is transported within luids (gases and liquids), linear momentum is also associated with transport,

More information

Where does Bernoulli's Equation come from?

Where does Bernoulli's Equation come from? Where does Bernoulli's Equation come from? Introduction By now, you have seen the following equation many times, using it to solve simple fluid problems. P ρ + v + gz = constant (along a streamline) This

More information

1 One-dimensional analysis

1 One-dimensional analysis One-dimensional analysis. Introduction The simplest models for gas liquid flow systems are ones for which the velocity is uniform over a cross-section and unidirectional. This includes flows in a long

More information

Department of Physics

Department of Physics Department of Physics PHYS101-051 FINAL EXAM Test Code: 100 Tuesday, 4 January 006 in Building 54 Exam Duration: 3 hrs (from 1:30pm to 3:30pm) Name: Student Number: Section Number: Page 1 1. A car starts

More information

Fundamentals of Fluid Dynamics: Elementary Viscous Flow

Fundamentals of Fluid Dynamics: Elementary Viscous Flow Fundamentals of Fluid Dynamics: Elementary Viscous Flow Introductory Course on Multiphysics Modelling TOMASZ G. ZIELIŃSKI bluebox.ippt.pan.pl/ tzielins/ Institute of Fundamental Technological Research

More information

P = 1 3 (σ xx + σ yy + σ zz ) = F A. It is created by the bombardment of the surface by molecules of fluid.

P = 1 3 (σ xx + σ yy + σ zz ) = F A. It is created by the bombardment of the surface by molecules of fluid. CEE 3310 Thermodynamic Properties, Aug. 27, 2010 11 1.4 Review A fluid is a substance that can not support a shear stress. Liquids differ from gasses in that liquids that do not completely fill a container

More information

VIRTUE / WP4 Delft Twisted Foil in steady flow Simulation with EOLE

VIRTUE / WP4 Delft Twisted Foil in steady flow Simulation with EOLE 6 th Framework Programme "Sustainable development, global change and ecosystems" Project No. 516201 / WP4 Delft Twisted Foil in steady flow Simulation with EOLE Workshop Oct. 17-18, 2007 R. Marcer Principia

More information

Dynamic Meteorology - Introduction

Dynamic Meteorology - Introduction Dynamic Meteorology - Introduction Atmospheric dynamics the study of atmospheric motions that are associated with weather and climate We will consider the atmosphere to be a continuous fluid medium, or

More information

Fluid Statics. Pressure. Pressure

Fluid Statics. Pressure. Pressure Pressure Fluid Statics Variation of Pressure with Position in a Fluid Measurement of Pressure Hydrostatic Thrusts on Submerged Surfaces Plane Surfaces Curved Surfaces ddendum First and Second Moment of

More information

CHAPTER 4 BOUNDARY LAYER FLOW APPLICATION TO EXTERNAL FLOW

CHAPTER 4 BOUNDARY LAYER FLOW APPLICATION TO EXTERNAL FLOW CHAPTER 4 BOUNDARY LAYER FLOW APPLICATION TO EXTERNAL FLOW 4.1 Introduction Boundary layer concept (Prandtl 1904): Eliminate selected terms in the governing equations Two key questions (1) What are the

More information

Q1 Give answers to all of the following questions (5 marks each):

Q1 Give answers to all of the following questions (5 marks each): FLUID MECHANICS First Year Exam Solutions 03 Q Give answers to all of the following questions (5 marks each): (a) A cylinder of m in diameter is made with material of relative density 0.5. It is moored

More information

vector H. If O is the point about which moments are desired, the angular moment about O is given:

vector H. If O is the point about which moments are desired, the angular moment about O is given: The angular momentum A control volume analysis can be applied to the angular momentum, by letting B equal to angularmomentum vector H. If O is the point about which moments are desired, the angular moment

More information

2013/5/22. ( + ) ( ) = = momentum outflow rate. ( x) FPressure. 9.3 Nozzles. δ q= heat added into the fluid per unit mass

2013/5/22. ( + ) ( ) = = momentum outflow rate. ( x) FPressure. 9.3 Nozzles. δ q= heat added into the fluid per unit mass 9.3 Nozzles (b) omentum conservation : (i) Governing Equations Consider: nonadiabatic ternal (body) force ists variable flow area continuously varying flows δq f ternal force per unit volume +d δffdx dx

More information

Heat-fluid Coupling Simulation of Wet Friction Clutch

Heat-fluid Coupling Simulation of Wet Friction Clutch 3rd International Conerence on Mechatronics, Robotics and Automation (ICMRA 2015) Heat-luid Coupling Simulation o Wet Friction Clutch Tengjiao Lin 1,a *, Qing Wang 1, b, Quancheng Peng 1,c and Yan Xie

More information

Laminar Flow. Chapter ZERO PRESSURE GRADIENT

Laminar Flow. Chapter ZERO PRESSURE GRADIENT Chapter 2 Laminar Flow 2.1 ZERO PRESSRE GRADIENT Problem 2.1.1 Consider a uniform flow of velocity over a flat plate of length L of a fluid of kinematic viscosity ν. Assume that the fluid is incompressible

More information

CHAPTER (2) FLUID PROPERTIES SUMMARY DR. MUNZER EBAID MECH.ENG.DEPT.

CHAPTER (2) FLUID PROPERTIES SUMMARY DR. MUNZER EBAID MECH.ENG.DEPT. CHAPTER () SUMMARY DR. MUNZER EBAID MECH.ENG.DEPT. 08/1/010 DR.MUNZER EBAID 1 System Is defined as a given quantity of matter. Extensive Property Can be identified when it is Dependent on the total mass

More information

Consider a volume Ω enclosing a mass M and bounded by a surface δω. d dt. q n ds. The Work done by the body on the surroundings is.

Consider a volume Ω enclosing a mass M and bounded by a surface δω. d dt. q n ds. The Work done by the body on the surroundings is. The Energy Balance Consider a volume Ω enclosing a mass M and bounded by a surface δω. δω At a point x, the density is ρ, the local velocity is v, and the local Energy density is U. U v The rate of change

More information

Real Flows (continued)

Real Flows (continued) al Flows (continued) So ar we have talked about internal lows ideal lows (Poiseuille low in a tube) real lows (turbulent low in a tube) Strategy or handling real lows: How did we arrive at correlations?

More information

MA3D1 Fluid Dynamics Support Class 5 - Shear Flows and Blunt Bodies

MA3D1 Fluid Dynamics Support Class 5 - Shear Flows and Blunt Bodies MA3D1 Fluid Dynamics Support Class 5 - Shear Flows and Blunt Bodies 13th February 2015 Jorge Lindley email: J.V.M.Lindley@warwick.ac.uk 1 2D Flows - Shear flows Example 1. Flow over an inclined plane A

More information

Chapter 4: Fundamental Forces

Chapter 4: Fundamental Forces Chapter 4: Fundamental Forces Newton s Second Law: F=ma In atmospheric science it is typical to consider the force per unit mass acting on the atmosphere: Force mass = a In order to understand atmospheric

More information

University of Hail Faculty of Engineering DEPARTMENT OF MECHANICAL ENGINEERING. ME Fluid Mechanics Lecture notes. Chapter 1

University of Hail Faculty of Engineering DEPARTMENT OF MECHANICAL ENGINEERING. ME Fluid Mechanics Lecture notes. Chapter 1 University of Hail Faculty of Engineering DEPARTMENT OF MECHANICAL ENGINEERING ME 311 - Fluid Mechanics Lecture notes Chapter 1 Introduction and fluid properties Prepared by : Dr. N. Ait Messaoudene Based

More information

Mathematical Modeling and response analysis of mechanical systems are the subjects of this chapter.

Mathematical Modeling and response analysis of mechanical systems are the subjects of this chapter. Chapter 3 Mechanical Systems A. Bazoune 3.1 INRODUCION Mathematical Modeling and response analysis of mechanical systems are the subjects of this chapter. 3. MECHANICAL ELEMENS Any mechanical system consists

More information

Computer Fluid Dynamics E181107

Computer Fluid Dynamics E181107 Computer Fluid Dynamics E181107 2181106 Transport equations, Navier Stokes equations Remark: foils with black background could be skipped, they are aimed to the more advanced courses Rudolf Žitný, Ústav

More information

Fluid Mechanics Discussion. Prepared By: Dr.Khalil M. Al-Astal Eng.Ahmed S. Al-Agha Eng.Ruba M. Awad

Fluid Mechanics Discussion. Prepared By: Dr.Khalil M. Al-Astal Eng.Ahmed S. Al-Agha Eng.Ruba M. Awad Discussion Prepared By: Dr.Khalil M. Al-Astal Eng.Ahmed S. Al-Agha Eng.Ruba M. Awad 2014-2015 Chapter (1) Fluids and their Properties Fluids and their Properties Fluids (Liquids or gases) which a substance

More information

Aerodynamics. Basic Aerodynamics. Continuity equation (mass conserved) Some thermodynamics. Energy equation (energy conserved)

Aerodynamics. Basic Aerodynamics. Continuity equation (mass conserved) Some thermodynamics. Energy equation (energy conserved) Flow with no friction (inviscid) Aerodynamics Basic Aerodynamics Continuity equation (mass conserved) Flow with friction (viscous) Momentum equation (F = ma) 1. Euler s equation 2. Bernoulli s equation

More information

1. Introduction, fluid properties (1.1, 2.8, 4.1, and handouts)

1. Introduction, fluid properties (1.1, 2.8, 4.1, and handouts) 1. Introduction, fluid properties (1.1, 2.8, 4.1, and handouts) Introduction, general information Course overview Fluids as a continuum Density Compressibility Viscosity Exercises: A1 Fluid mechanics Fluid

More information

Bernoulli and Pipe Flow

Bernoulli and Pipe Flow Civil Engineering Hydraulics Mechanics of Fluids Head Loss Calculations Bernoulli and The Bernoulli equation that we worked with was a bit simplistic in the way it looked at a fluid system All real systems

More information

Basic concepts in viscous flow

Basic concepts in viscous flow Élisabeth Guazzelli and Jeffrey F. Morris with illustrations by Sylvie Pic Adapted from Chapter 1 of Cambridge Texts in Applied Mathematics 1 The fluid dynamic equations Navier-Stokes equations Dimensionless

More information

Pressure in stationary and moving fluid. Lab-On-Chip: Lecture 2

Pressure in stationary and moving fluid. Lab-On-Chip: Lecture 2 Pressure in stationary and moving fluid Lab-On-Chip: Lecture Fluid Statics No shearing stress.no relative movement between adjacent fluid particles, i.e. static or moving as a single block Pressure at

More information

SYSTEMS VS. CONTROL VOLUMES. Control volume CV (open system): Arbitrary geometric space, surrounded by control surfaces (CS)

SYSTEMS VS. CONTROL VOLUMES. Control volume CV (open system): Arbitrary geometric space, surrounded by control surfaces (CS) SYSTEMS VS. CONTROL VOLUMES System (closed system): Predefined mass m, surrounded by a system boundary Control volume CV (open system): Arbitrary geometric space, surrounded by control surfaces (CS) Many

More information

Physics for Scientists and Engineers. Chapter 6 Dynamics I: Motion Along a Line

Physics for Scientists and Engineers. Chapter 6 Dynamics I: Motion Along a Line Physics for Scientists and Engineers Chapter 6 Dynamics I: Motion Along a Line Spring, 008 Ho Jung Paik Applications of Newton s Law Objects can be modeled as particles Masses of strings or ropes are negligible

More information

RESOLUTION MSC.362(92) (Adopted on 14 June 2013) REVISED RECOMMENDATION ON A STANDARD METHOD FOR EVALUATING CROSS-FLOODING ARRANGEMENTS

RESOLUTION MSC.362(92) (Adopted on 14 June 2013) REVISED RECOMMENDATION ON A STANDARD METHOD FOR EVALUATING CROSS-FLOODING ARRANGEMENTS (Adopted on 4 June 203) (Adopted on 4 June 203) ANNEX 8 (Adopted on 4 June 203) MSC 92/26/Add. Annex 8, page THE MARITIME SAFETY COMMITTEE, RECALLING Article 28(b) o the Convention on the International

More information

Work Up an Incline. Work = Force x Distance. Push up: 1500J. What is the PE at the top? mg = 500N. An incline is a simple machine!

Work Up an Incline. Work = Force x Distance. Push up: 1500J. What is the PE at the top? mg = 500N. An incline is a simple machine! Quick Question Work Up an Incline The block o ice weighs 500 Newtons. How much work does it take to push it up the incline compared to liting it straight up? Ignore riction. Work Up an Incline Work = Force

More information

Exercise 5: Exact Solutions to the Navier-Stokes Equations I

Exercise 5: Exact Solutions to the Navier-Stokes Equations I Fluid Mechanics, SG4, HT009 September 5, 009 Exercise 5: Exact Solutions to the Navier-Stokes Equations I Example : Plane Couette Flow Consider the flow of a viscous Newtonian fluid between two parallel

More information

Introduction to nomenclature. Two-phase flow regimes in vertical tubes. Forced convective boiling: Regions of boiling and flow

Introduction to nomenclature. Two-phase flow regimes in vertical tubes. Forced convective boiling: Regions of boiling and flow NTEC Module: Water Reactor Performance and Safety Two-phase flow regimes in vertical tubes ecture 5: Introduction to two-phase flow. F. ewitt Imperial College ondon Bubble Flow Slug or Plug Flow Churn

More information

Lagrangian description from the perspective of a parcel moving within the flow. Streamline Eulerian, tangent line to instantaneous velocity field.

Lagrangian description from the perspective of a parcel moving within the flow. Streamline Eulerian, tangent line to instantaneous velocity field. Chapter 2 Hydrostatics 2.1 Review Eulerian description from the perspective of fixed points within a reference frame. Lagrangian description from the perspective of a parcel moving within the flow. Streamline

More information

MM303 FLUID MECHANICS I PROBLEM SET 1 (CHAPTER 2) FALL v=by 2 =-6 (1/2) 2 = -3/2 m/s

MM303 FLUID MECHANICS I PROBLEM SET 1 (CHAPTER 2) FALL v=by 2 =-6 (1/2) 2 = -3/2 m/s MM303 FLUID MECHANICS I PROBLEM SET 1 (CHAPTER ) FALL 018 1) For the velocity fields given below, determine: i) Whether the flow field is one-, two-, or three-dimensional, and why. ii) Whether the flow

More information

ASSIGNMENT COVER SHEET omicron

ASSIGNMENT COVER SHEET omicron ASSIGNMENT COVER SHEET omicron Name Question Done Backpack Ready for test Drill A differentiation Drill B sketches Drill C Partial fractions Drill D integration Drill E differentiation Section A integration

More information

Total energy in volume

Total energy in volume General Heat Transfer Equations (Set #3) ChE 1B Fundamental Energy Postulate time rate of change of internal +kinetic energy = rate of heat transfer + surface work transfer (viscous & other deformations)

More information

g (z) = 1 (1 + z/a) = 1 1 ( km/10 4 km) 2

g (z) = 1 (1 + z/a) = 1 1 ( km/10 4 km) 2 1.4.2 Gravitational Force g is the gravitational force. It always points towards the center of mass, and it is proportional to the inverse square of the distance above the center of mass: g (z) = GM (a

More information

Soft Bodies. Good approximation for hard ones. approximation breaks when objects break, or deform. Generalization: soft (deformable) bodies

Soft Bodies. Good approximation for hard ones. approximation breaks when objects break, or deform. Generalization: soft (deformable) bodies Soft-Body Physics Soft Bodies Realistic objects are not purely rigid. Good approximation for hard ones. approximation breaks when objects break, or deform. Generalization: soft (deformable) bodies Deformed

More information

Fluid Dynamics Exam #1: Introduction, fluid statics, and the Bernoulli equation March 2, 2016, 7:00 p.m. 8:40 p.m. in CE 118

Fluid Dynamics Exam #1: Introduction, fluid statics, and the Bernoulli equation March 2, 2016, 7:00 p.m. 8:40 p.m. in CE 118 CVEN 311-501 (Socolofsky) Fluid Dynamics Exam #1: Introduction, fluid statics, and the Bernoulli equation March 2, 2016, 7:00 p.m. 8:40 p.m. in CE 118 Name: : UIN: : Instructions: Fill in your name and

More information

Chapter 8 Laminar Flows with Dependence on One Dimension

Chapter 8 Laminar Flows with Dependence on One Dimension Chapter 8 Laminar Flows with Dependence on One Dimension Couette low Planar Couette low Cylindrical Couette low Planer rotational Couette low Hele-Shaw low Poiseuille low Friction actor and Reynolds number

More information

Uniform Channel Flow Basic Concepts. Definition of Uniform Flow

Uniform Channel Flow Basic Concepts. Definition of Uniform Flow Uniform Channel Flow Basic Concepts Hydromechanics VVR090 Uniform occurs when: Definition of Uniform Flow 1. The depth, flow area, and velocity at every cross section is constant 2. The energy grade line,

More information

PROCESS SYSTEMS ENGINEERING Dr.-Ing. Richard Hanke-Rauschenbach

PROCESS SYSTEMS ENGINEERING Dr.-Ing. Richard Hanke-Rauschenbach Otto-von-Guerice University Magdeburg PROCESS SYSTEMS ENGINEERING Dr.-Ing. Richard Hane-Rauschenbach Project wor No. 1, Winter term 2011/2012 Sample Solution Delivery of the project handout: Wednesday,

More information

TABLE OF CONTENTS CHAPTER TITLE PAGE

TABLE OF CONTENTS CHAPTER TITLE PAGE v TABLE OF CONTENTS CHAPTER TITLE PAGE TABLE OF CONTENTS LIST OF TABLES LIST OF FIGURES LIST OF SYMBOLS LIST OF APPENDICES v viii ix xii xiv CHAPTER 1 INTRODUCTION 1.1 Introduction 1 1.2 Literature Review

More information

Lectures on Applied Reactor Technology and Nuclear Power Safety. Lecture No 7

Lectures on Applied Reactor Technology and Nuclear Power Safety. Lecture No 7 ectures on Nuclear Power Safety ecture No 7 itle: hermal-hydraulic nalysis of Single-Phase lows in Heated hannels Department of Energy echnology KH Spring 005 Slide No Outline of the ecture lad-oolant

More information

When water (fluid) flows in a pipe, for example from point A to point B, pressure drop will occur due to the energy losses (major and minor losses).

When water (fluid) flows in a pipe, for example from point A to point B, pressure drop will occur due to the energy losses (major and minor losses). PRESSURE DROP AND OSSES IN PIPE When water (luid) lows in a pipe, or example rom point A to point B, pressure drop will occur due to the energy losses (major and minor losses). A B Bernoulli equation:

More information

Fundamental Concepts of Convection : Flow and Thermal Considerations. Chapter Six and Appendix D Sections 6.1 through 6.8 and D.1 through D.

Fundamental Concepts of Convection : Flow and Thermal Considerations. Chapter Six and Appendix D Sections 6.1 through 6.8 and D.1 through D. Fundamental Concepts of Convection : Flow and Thermal Considerations Chapter Six and Appendix D Sections 6.1 through 6.8 and D.1 through D.3 6.1 Boundary Layers: Physical Features Velocity Boundary Layer

More information

Chapter 1. Continuum mechanics review. 1.1 Definitions and nomenclature

Chapter 1. Continuum mechanics review. 1.1 Definitions and nomenclature Chapter 1 Continuum mechanics review We will assume some familiarity with continuum mechanics as discussed in the context of an introductory geodynamics course; a good reference for such problems is Turcotte

More information

Civil Engineering Hydraulics Mechanics of Fluids. Pressure and Fluid Statics. The fastest healing part of the body is the tongue.

Civil Engineering Hydraulics Mechanics of Fluids. Pressure and Fluid Statics. The fastest healing part of the body is the tongue. Civil Engineering Hydraulics Mechanics of Fluids and Fluid Statics The fastest healing part of the body is the tongue. Common Units 2 In order to be able to discuss and analyze fluid problems we need to

More information

PROPOSAL OF HEAT EXCHANGER IN MICRO COGENERATION UNIT, CONFIGURATION WITH BIOMASS COMBUSTION. Jozef HUŽVÁR, Patrik NEMEC

PROPOSAL OF HEAT EXCHANGER IN MICRO COGENERATION UNIT, CONFIGURATION WITH BIOMASS COMBUSTION. Jozef HUŽVÁR, Patrik NEMEC PROPOSAL OF HEAT EXCHANGER IN MICRO COGENERATION UNIT, CONFIGURATION WITH BIOMASS COMBUSTION Jozef HUŽVÁR, Patri NEMEC Authors: Worplace: Jozef Hužvár, MSc. Eng. Patri Nemec, MSc. Eng. Faculty of Mechanical

More information

Dynamics of the Mantle and Lithosphere ETH Zürich Continuum Mechanics in Geodynamics: Equation cheat sheet

Dynamics of the Mantle and Lithosphere ETH Zürich Continuum Mechanics in Geodynamics: Equation cheat sheet Dynamics of the Mantle and Lithosphere ETH Zürich Continuum Mechanics in Geodynamics: Equation cheat sheet or all equations you will probably ever need Definitions 1. Coordinate system. x,y,z or x 1,x

More information

Pressure in stationary and moving fluid Lab- Lab On- On Chip: Lecture 2

Pressure in stationary and moving fluid Lab- Lab On- On Chip: Lecture 2 Pressure in stationary and moving fluid Lab-On-Chip: Lecture Lecture plan what is pressure e and how it s distributed in static fluid water pressure in engineering problems buoyancy y and archimedes law;

More information

Consider a volume Ω enclosing a mass M and bounded by a surface δω. d dt. q n ds. The Work done by the body on the surroundings is

Consider a volume Ω enclosing a mass M and bounded by a surface δω. d dt. q n ds. The Work done by the body on the surroundings is The Energy Balance Consider a volume enclosing a mass M and bounded by a surface δ. δ At a point x, the density is ρ, the local velocity is v, and the local Energy density is U. U v The rate of change

More information

ME Machine Design I

ME Machine Design I ME 5 - Machine Design I Summer Semester 008 Name Lab. Div. EXAM. OEN BOOK AND CLOSED NOTES. Wednesday, July 16th, 008 Write your solutions on the blank paper that is provided. Write on one side of the

More information

CFD Analysis for Thermal Behavior of Turbulent Channel Flow of Different Geometry of Bottom Plate

CFD Analysis for Thermal Behavior of Turbulent Channel Flow of Different Geometry of Bottom Plate International Journal Of Engineering Research And Development e-issn: 2278-067X, p-issn: 2278-800X, www.ijerd.com Volume 13, Issue 9 (September 2017), PP.12-19 CFD Analysis for Thermal Behavior of Turbulent

More information

Chapter 1: Mathematical Concepts and Vectors

Chapter 1: Mathematical Concepts and Vectors Chapter 1: Mathematical Concepts and Vectors giga G 1 9 mega M 1 6 kilo k 1 3 centi c 1 - milli m 1-3 micro μ 1-6 nano n 1-9 1 in =.54 cm 1 m = 1 cm = 3.81 t 1 mi = 58 t = 169 m 1 hr = 36 s 1 day = 86,4

More information

Turbomachinery & Turbulence. Lecture 2: One dimensional thermodynamics.

Turbomachinery & Turbulence. Lecture 2: One dimensional thermodynamics. Turbomachinery & Turbulence. Lecture 2: One dimensional thermodynamics. F. Ravelet Laboratoire DynFluid, Arts et Metiers-ParisTech February 3, 2016 Control volume Global balance equations in open systems

More information

Boundary layer flows The logarithmic law of the wall Mixing length model for turbulent viscosity

Boundary layer flows The logarithmic law of the wall Mixing length model for turbulent viscosity Boundary layer flows The logarithmic law of the wall Mixing length model for turbulent viscosity Tobias Knopp D 23. November 28 Reynolds averaged Navier-Stokes equations Consider the RANS equations with

More information

On side wall labeled A: we can express the pressure in a Taylor s series expansion: x 2. + higher order terms,

On side wall labeled A: we can express the pressure in a Taylor s series expansion: x 2. + higher order terms, Chapter 1 Notes A Note About Coordinates We nearly always use a coordinate system in this class where the vertical, ˆk, is normal to the Earth s surface and the x-direction, î, points to the east and the

More information

Finite difference models: one dimension

Finite difference models: one dimension Chapter 6 Finite difference models: one dimension 6.1 overview Our goal in building numerical models is to represent differential equations in a computationally manageable way. A large class of numerical

More information

Continuum mechanism: Stress and strain

Continuum mechanism: Stress and strain Continuum mechanics deals with the relation between forces (stress, σ) and deformation (strain, ε), or deformation rate (strain rate, ε). Solid materials, rigid, usually deform elastically, that is the

More information

Sourabh V. Apte. 308 Rogers Hall

Sourabh V. Apte. 308 Rogers Hall Sourabh V. Apte 308 Rogers Hall sva@engr.orst.edu 1 Topics Quick overview of Fluid properties, units Hydrostatic forces Conservation laws (mass, momentum, energy) Flow through pipes (friction loss, Moody

More information

Numerical Simulations of a Stratified Oceanic Bottom Boundary Layer. John R. Taylor - MIT Advisor: Sutanu Sarkar - UCSD

Numerical Simulations of a Stratified Oceanic Bottom Boundary Layer. John R. Taylor - MIT Advisor: Sutanu Sarkar - UCSD Numerical Simulations of a Stratified Oceanic Bottom Boundary Layer John R. Taylor - MIT Advisor: Sutanu Sarkar - UCSD Motivation Objective I: Assess and improve parameterizations of the bottom boundary

More information

Consider a control volume in the form of a straight section of a streamtube ABCD.

Consider a control volume in the form of a straight section of a streamtube ABCD. 6 MOMENTUM EQUATION 6.1 Momentum and Fluid Flow In mechanics, the momentum of a particle or object is defined as the product of its mass m and its velocity v: Momentum = mv The particles of a fluid stream

More information

Review of fluid dynamics

Review of fluid dynamics Chapter 2 Review of fluid dynamics 2.1 Preliminaries ome basic concepts: A fluid is a substance that deforms continuously under stress. A Material olume is a tagged region that moves with the fluid. Hence

More information

Reynolds, an engineering professor in early 1880 demonstrated two different types of flow through an experiment:

Reynolds, an engineering professor in early 1880 demonstrated two different types of flow through an experiment: 7 STEADY FLOW IN PIPES 7.1 Reynolds Number Reynolds, an engineering professor in early 1880 demonstrated two different types of flow through an experiment: Laminar flow Turbulent flow Reynolds apparatus

More information

ASSESSMENT OF AN INTERFACIAL SHEAR TERM FOR ADIABATIC DISPERSED AIR-WATER TWO-PHASE FLOW WITH THE TWO-FLUID MODEL

ASSESSMENT OF AN INTERFACIAL SHEAR TERM FOR ADIABATIC DISPERSED AIR-WATER TWO-PHASE FLOW WITH THE TWO-FLUID MODEL ASSESSMEN OF AN INERFACIAL SHEAR ERM FOR ADIABAIC DISPERSED AIR-WAER WO-PHASE FLOW WIH HE WO-FLUID MODEL S. L. Sharma,. Hibii, M. Ishii School o Nuclear Engineering, Purdue University 400 Central Dr.,

More information

2015 American Journal of Engineering Research (AJER)

2015 American Journal of Engineering Research (AJER) American Journal o Engineering Research (AJER) 2015 American Journal o Engineering Research (AJER) e-issn: 2320-0847 p-issn : 2320-0936 Volume-4, Issue-7, pp-33-40.ajer.org Research Paper Open Access The

More information

Basic equations of motion in fluid mechanics

Basic equations of motion in fluid mechanics 1 Annex 1 Basic equations of motion in fluid mechanics 1.1 Introduction It is assumed that the reader of this book is familiar with the basic laws of fluid mechanics. Nevertheless some of these laws will

More information

Chapter 8: Flow in Pipes

Chapter 8: Flow in Pipes 8-1 Introduction 8-2 Laminar and Turbulent Flows 8-3 The Entrance Region 8-4 Laminar Flow in Pipes 8-5 Turbulent Flow in Pipes 8-6 Fully Developed Pipe Flow 8-7 Minor Losses 8-8 Piping Networks and Pump

More information

Summary of the Equations of Fluid Dynamics

Summary of the Equations of Fluid Dynamics Reference: Summary of the Equations of Fluid Dynamics Fluid Mechanics, L.D. Landau & E.M. Lifshitz 1 Introduction Emission processes give us diagnostics with which to estimate important parameters, such

More information