Chapter 5: Control Volume Approach and Continuity Principle Dr Ali Jawarneh

Similar documents
Second Law. first draft 9/23/04, second Sept Oct 2005 minor changes 2006, used spell check, expanded example

MECHANICAL PROPERTIES OF FLUIDS NCERT

CHBE320 LECTURE IV MATHEMATICAL MODELING OF CHEMICAL PROCESS. Professor Dae Ryook Yang

CHE302 LECTURE IV MATHEMATICAL MODELING OF CHEMICAL PROCESS. Professor Dae Ryook Yang

Physics 235 Chapter 2. Chapter 2 Newtonian Mechanics Single Particle

Chapter 7 Response of First-order RL and RC Circuits

Chemical Engineering Thermodynamics

LAPLACE TRANSFORM AND TRANSFER FUNCTION

Math Week 14 April 16-20: sections first order systems of linear differential equations; 7.4 mass-spring systems.

15. Vector Valued Functions

Math 333 Problem Set #2 Solution 14 February 2003

Module 2 F c i k c s la l w a s o s f dif di fusi s o i n

1. VELOCITY AND ACCELERATION

1998 Calculus AB Scoring Guidelines

Introduction to Probability and Statistics Slides 4 Chapter 4

AP CALCULUS AB 2003 SCORING GUIDELINES (Form B)

Reliability of Technical Systems

ACCUMULATION. Section 7.5 Calculus AP/Dual, Revised /26/2018 7:27 PM 7.5A: Accumulation 1

From Particles to Rigid Bodies

ENV 6015 Solution to Mixing Problem Set

IB Physics Kinematics Worksheet

Mathcad Lecture #7 In-class Worksheet "Smart" Solve Block Techniques Handout

RTT relates between the system approach with finite control volume approach for a system property:

2.1: What is physics? Ch02: Motion along a straight line. 2.2: Motion. 2.3: Position, Displacement, Distance

Linear Surface Gravity Waves 3., Dispersion, Group Velocity, and Energy Propagation

Equations of motion for constant acceleration

WEEK-3 Recitation PHYS 131. of the projectile s velocity remains constant throughout the motion, since the acceleration a x

Variable acceleration, Mixed Exercise 11

Diffusion & Viscosity: Navier-Stokes Equation

Exam 1 Solutions. 1 Question 1. February 10, Part (A) 1.2 Part (B) To find equilibrium solutions, set P (t) = C = dp

Announcements: Warm-up Exercise:

MAE143A Signals & Systems - Homework 2, Winter 2014 due by the end of class Thursday January 23, 2014.

Sub Module 2.6. Measurement of transient temperature

3, so θ = arccos

Lecture 20: Riccati Equations and Least Squares Feedback Control

Direct Current Circuits. February 19, 2014 Physics for Scientists & Engineers 2, Chapter 26 1

Course II. Lesson 7 Applications to Physics. 7A Velocity and Acceleration of a Particle

Ground Rules. PC1221 Fundamentals of Physics I. Kinematics. Position. Lectures 3 and 4 Motion in One Dimension. A/Prof Tay Seng Chuan

1 1 + x 2 dx. tan 1 (2) = ] ] x 3. Solution: Recall that the given integral is improper because. x 3. 1 x 3. dx = lim dx.

Week 1 Lecture 2 Problems 2, 5. What if something oscillates with no obvious spring? What is ω? (problem set problem)

PHYS 1401 General Physics I Test 3 Review Questions

PROBLEMS FOR MATH 162 If a problem is starred, all subproblems are due. If only subproblems are starred, only those are due. SLOPES OF TANGENT LINES

Theory of! Partial Differential Equations!

Theory of! Partial Differential Equations-I!

System of Linear Differential Equations

Solutions from Chapter 9.1 and 9.2

Lecture 2-1 Kinematics in One Dimension Displacement, Velocity and Acceleration Everything in the world is moving. Nothing stays still.

f(s)dw Solution 1. Approximate f by piece-wise constant left-continuous non-random functions f n such that (f(s) f n (s)) 2 ds 0.

Solutions to Assignment 1

BEng (Hons) Telecommunications. Examinations for / Semester 2

EXERCISES FOR SECTION 1.5

Module 3: The Damped Oscillator-II Lecture 3: The Damped Oscillator-II

v x + v 0 x v y + a y + v 0 y + 2a y + v y Today: Projectile motion Soccer problem Firefighter example

ME 391 Mechanical Engineering Analysis

Chapter 2. First Order Scalar Equations

R.#W.#Erickson# Department#of#Electrical,#Computer,#and#Energy#Engineering# University#of#Colorado,#Boulder#

AP CALCULUS AB 2003 SCORING GUIDELINES (Form B)

Chapter 15: Phenomena. Chapter 15 Chemical Kinetics. Reaction Rates. Reaction Rates R P. Reaction Rates. Rate Laws

4. Electric field lines with respect to equipotential surfaces are

APPM 2360 Homework Solutions, Due June 10

EE 315 Notes. Gürdal Arslan CLASS 1. (Sections ) What is a signal?

2. Nonlinear Conservation Law Equations

Chapter 5 Control Volume Approach and Continuity Equation

Chapter 6 Differential Analysis of Fluid Flow

Hamilton Jacobi equations

t is a basis for the solution space to this system, then the matrix having these solutions as columns, t x 1 t, x 2 t,... x n t x 2 t...

The law of conservation of mass: Mass can be neither created nor destroyed. It can only be transported or stored.

Design of a control system

Unsteady Mass- Transfer Models

t 2 B F x,t n dsdt t u x,t dxdt

Math 334 Test 1 KEY Spring 2010 Section: 001. Instructor: Scott Glasgow Dates: May 10 and 11.

Exam I. Name. Answer: a. W B > W A if the volume of the ice cubes is greater than the volume of the water.

Simulating models with heterogeneous agents

Chapter 8 The Complete Response of RL and RC Circuits

Class Meeting # 10: Introduction to the Wave Equation

Hamilton- J acobi Equation: Explicit Formulas In this lecture we try to apply the method of characteristics to the Hamilton-Jacobi equation: u t

1 Solutions to selected problems

Suggested Practice Problems (set #2) for the Physics Placement Test

Lecture Outline. Introduction Transmission Line Equations Transmission Line Wave Equations 8/10/2018. EE 4347 Applied Electromagnetics.

Chapter 2: Principles of steady-state converter analysis

4.6 One Dimensional Kinematics and Integration

In this chapter the model of free motion under gravity is extended to objects projected at an angle. When you have completed it, you should

3.1.3 INTRODUCTION TO DYNAMIC OPTIMIZATION: DISCRETE TIME PROBLEMS. A. The Hamiltonian and First-Order Conditions in a Finite Time Horizon

- If one knows that a magnetic field has a symmetry, one may calculate the magnitude of B by use of Ampere s law: The integral of scalar product

copper ring magnetic field

PHYSICS 220 Lecture 02 Motion, Forces, and Newton s Laws Textbook Sections

2.3 SCHRÖDINGER AND HEISENBERG REPRESENTATIONS

Calculation of the Two High Voltage Transmission Line Conductors Minimum Distance

Designing Information Devices and Systems I Spring 2019 Lecture Notes Note 17

Math 334 Fall 2011 Homework 11 Solutions

Applications of the Basic Equations Chapter 3. Paul A. Ullrich

CHAPTER 12 DIRECT CURRENT CIRCUITS

Chapter 7: Inverse-Response Systems

Fluid Flows and Bernoulli s Principle

Continuous Time. Time-Domain System Analysis. Impulse Response. Impulse Response. Impulse Response. Impulse Response. ( t) + b 0.

Solutions of Sample Problems for Third In-Class Exam Math 246, Spring 2011, Professor David Levermore

Vanishing Viscosity Method. There are another instructive and perhaps more natural discontinuous solutions of the conservation law

Summary of shear rate kinematics (part 1)

EECE 301 Signals & Systems Prof. Mark Fowler

Transcription:

Chaper 5: Conrol Volume Approach and Coninuiy Principle By Dr Ali Jawarneh Deparmen of Mechanical Engineering Hashemie Universiy 1

Ouline Rae of Flow Conrol volume approach. Conservaion of mass he coninuiy equaion. Caviaions Differenial form of he coninuiy equaion 2

5.1: Rae of flow - Discharge or Volume flow rae, Q {m 3 /s} For a fluid wih consan velociy: Q V.A The do produc means ha he velociy componen normal o he area For a fluid wih variable velociy: m Q - Mass Flow Rae,, {kg/s} Consan velociy Variable velociy and consan densiy m& V.A m& V.dAQ V.dA - Mean Velociy VV avg Q /A 3

Example: Find he volume and mass flow rae of waer. Soluion: π Q VA V 4 D 2 10 π 0. 01 4 2 7. 85 10 4 m QQ 1000 7. 85 10 4 0. 785 k/ kg/s 4 m 3 /s Example: Find he volume and mass flow rae of waer. Soluion: Q VAcos 30 6. 798 10 m o 4 3 /s m Q 0. 679 kg/s 4

Example: The recangular channel is 2 m wide. Wha is he discharge in he channel? Soluion: Q A V.dA y x 0 0 0 0 Vdxdy Q 1 / 3 V.dA y 2dy A 1cos 30 If he case is pipe 0 o 1. 24 m 3 /s Q 1 r0 cos 30 2 V.dA V r 2 π A 0 o r dr 5

5.2: Conrol Volume Approach The mehod employed for solving mos problems in fluid mechanics is he conrol volume approach also known as he Reynolds Transpor Theorem. A conrol volume is a seleced volumeric region in space. A conrol surface is he surface enclosing he conrol volume. 6

The mass wihin he conrol volume can change wih ime, and a conrol volume can deform wih ime, and move and roae in space. In conras wih he conrol volume, a sysem is defined as a coninuous mass of fluid ha always conains he same fluid paricles. 7

A ime : M M Afer ime : sys M m& M m& ou ou in in 8

The mass of he sysem a ime : in ou sys M M M M m m M M M M & & m m M M M M in ou sys sys 9

Dividing by and aking he limi as 0: dm sys dm m& ou m& in dm sys By definiion: 0 Consequenly: dm m& in m& ou Coninuiy Equaion 10

Example: A ank has a hole in he boom wih a cross-secional secional area of 0.00250025 m 2. The cross-secional secional area of he ank is 0.1 m 2. The velociy of he liquid flowing ou he boom hole is V2gh 0.5, where h is he heigh of he waer surface in he ank above he oule. A a cerain ime he surface level in he ank is 1 m and rising i a he rae of 0.1 cm/s. The liquid id is incompressible. Find he velociy of he liquid hrough he inle. 11

Soluion: dh 0. 1 cm/s dm m in m M V Ah ou m in Vin A in m ou V Aou 2 gh dh A Vin Ain 2gh A A ou ou dm dh A 0. 1 0. 1/ 100 Vin 0. 0025 2 9. 81 1 0. 0025 V in 4. 468 m/s End of he soluion Exercise:Commen if we need o find he ime from h1 o h2: Example: dh/ 2h 12

Propery Transpor across he Conrol surface For seady, onedimensional flow in a condui: V. A V.A V.A cs 1 1 1 2 2 2 VA VA 2 2 2 1 1 1 For consan densiy incompressible flow: V.A V2A2 V1A 1 cs 13

Reynolds Transpor Theorem dbsys d b dv b VdA 14444244443 { cs Lagrangian Eulerian B bdm b dv 14

5.3: Coninuiy Equaion C Conservaion of fm Mass Depending on he previous analysis, i can be verified ha: dm sys d dv V. da And since he mass of a sysem is consan, hen: cs d V. d A dv cs dm For flow sreams having a uniform velociy across he flow secions: cs V. A m& in d dv m& ou 15

cs d V. da dv This equaion saes ha he rae of accumulaion of mass in he CV he ne mass efflux hrough he CS Ne efflux mass flow rae ou of he CV mass flow rae in he CV 16

Example: seady, incompressible flow of waer hrough he device. Given: A 1 0.2 m 2 A 2 0.2 m 2 A 3 0.15 m 2 V 1 5 m/s V 3 12 m/s Q 4 0.1 m 3 /s 999 kg/m 3 Find V 2 and i s direcion. 17

Soluion: 0.0 cs d V.dA dv V.dA 0. 0 V.A 0 cs V. A V. A V. A V. A 1 1 1 2 2 2 0. 0 since he problem is incompressible: cons 3 V 1. A1 V2. A2 V3. A3 V4. A4 0. 0 V A V A V A V A 0 0 1 1 2 2 3 3 4 4. V 1 A1 V2 A2 V3 A3 Q4 0. 0 3 5 0. 2 V2 0. 2 12 0. 15 0. 1 0. 0 V2 44. 5 m / s Because i is ve, he assumpion is no valid, so he V 2 goes inward he. 2 g 3 4 4 4 18

Example: Find he V max for he given seady, incompressible flow hrough pipe 3. Given: A 1 0.1 m 2 V 1 5 m/s A 2 0.1 m 2 V 2 3 m/s A 3 0.1256 m 2 19

Soluion: 0.0 V. cs d V.dA dv V.dA 0. 0 1 A1. cs o find V 3 : le V 3 a b r cs V2. A2 V3.dA3 0 0 V A V A V.dA 0 0 @r0, V 3 V max a V max, @rr o,v 3 0.0 r V 3 V max [1- r/r o ] 1 1 2 2 3 3. cs o r π 2 V3.dA3 Vmax 1 2πr dr ro Vmax r cs o o 3 π 2 A3 0. 1256 d 3 d 3 0. 4 m ro 0. 2 4 m π 2 5 0. 1 3 0. 1 0. 2 Vmax 0. 0 Vmax 3 19. 1 m/s b -V max /r o 20

Example: Tank of a volume of 0.05 m 3 conain air. A 0.0, 0 air escapes hrough a valve. Air leaves wih speed V300 m/s and densiy of 6 kg/m 3 hrough area of 65 mm 2. Find he rae of change of air densiy in he ank a 0.0. 21

Soluion: cs V.dA d dv Properies in he ank are uniform, bu ime dependence: 1 V 1 A 1 d f n dv d V V End of he soluion. Exercise: Solve he example ha appears in slide # 11 using his equaion: d d 3 2 d 1 V1 A1 6 300 65 10 3 2. 34 kg/m /s V 0.05 cs V.dA dv 22

Example: Air flows seadily beween wo secions in a long, sraigh porion of 4-in inside diameer pipe. The uniformly disribued emperaure and pressure a each secion are given. If he average air velociy nonuniform velociy disribuion a secion 2 is 1000 f/s, calculae he average air velociy a secion 1. 23

Soluion: 24

5.4: Caviaion - Caviaion is he phenomenon ha occur when he fluid pressure is reduced d o he local l vapor pressure -Under such condiions vapor bubbles form, grow, and hen collapse, producing shock wave, noise, and dynamics effecs ha lead o decreased equipmen performance and, frequenly, equipmen failure -Caviaion ypically occurs a locaions where he velociy is high -If he pipe area is reduced, he velociy is increased according o he coninuiy equaion and he pressure is reduced as dicaed by he Bernoulli equaion 25

- As he flow rae increases, he pressure a he resricion can become sub-amospheric. The pressure can drop no longer han he vapor pressure of he liquid because, a his poin, he liquid will boil and caviaion ensues. Formaion of vapor bubbles in he process of caviaion. i a Caviaion. b Caviaion higher flow rae. 26

A a given pressure, he emperaure a which a pure subsance changes phase is called he sauraion emperaure T sa. Likewise, a a given emperaure, he pressure a which a pure subsance changes phase is called he sauraion pressure P sa. A an absolue pressure of 1 sandard amosphere 1 am or 101.325 kpa, for example, he sauraion emperaure of waer is 100 C. Conversely, a a emperaure of 100 C, he sauraion pressure of waer is 1 am. The vapor pressure P v of a pure subsance is defined as he pressure exered by is vapor in phase equilibrium wih is liquid a a given emperaure. P v is a propery of he pure subsance, and urns ou o be idenical o he sauraion pressure Psa of he liquid P v P sa. 27

For phase-change processes beween he liquid and vapor phases of a pure subsance, he sauraion pressure and he vapor pressure are equivalen since he vapor is pure. Noe ha he pressure value would be he samewheher i is measured in he vapor or liquidid phase provided ha i is measured a a locaion close o he liquid vapor inerface o avoid he hydrosaic effecs. Vapor pressure increases wih emperaure. Thus, a subsance a higher emperaures boils a higher pressures. For example, waer boils a 134 C in a pressure cooker operaing a 3 am absolue pressure, bu i boils a 93 C in an ordinary pan a a 2000-m elevaion, where he amospheric pressure is 0.8 am. The sauraion or vapor pressures are given in Appendices for various subsances. A mini able for waer is given in following able for easy reference. 28

29

5.5: Differenial Form of he Coninuiy Equaion Coninuiy Equaion Applying he coninuiy equaion o a finie volume: cs d d V A V. z y x d y x w z x v z y u Dividing by he volume: 0 w v u 30 0 z w y v x u

When he volume approaches zero: pp 0 z w y v x u For seady flow: z y x w v u If he flow is incompressible: 0 z w y v x u If he flow is incompressible: 0 z w y v x u in vecor noaion: z y x 0 V. where is he Del operaor 31 k z j y i x operaor

Comparison beween he differenial and Comparison beween he differenial and inegral form of he coninuiy equaion. Differenial Form of he Coninuiy Equaion 0 w v u 0 z w y v x u Inegral Form of he Coninuiy Equaion cs dv d V.dA 32

Example: check he following equaion if i saisfies he coninuiy equaion for incompressible flow. Soluion: V u v 0 x y u u 2xy x v 2xy y x 2 y 2 i xy j i saisfies he coninuiy equaion. 33