M E 320 Professor John M. Cimbala Lecture 10. The Reynolds Transport Theorem (RTT) (Section 4-6)

Similar documents
M E 320 Professor John M. Cimbala Lecture 10

MOMENTUM PRINCIPLE. Review: Last time, we derived the Reynolds Transport Theorem: Chapter 6. where B is any extensive property (proportional to mass),

ME 3560 Fluid Mechanics

Chapter 6: Momentum Analysis

Differential relations for fluid flow

CE 204 FLUID MECHANICS

Chapter 6: Momentum Analysis of Flow Systems

Shell/Integral Balances (SIB)

Conservation of Angular Momentum

Chapter 4 Continuity Equation and Reynolds Transport Theorem

M E 320 Professor John M. Cimbala Lecture 24

Chapter 5 Control Volume Approach and Continuity Equation

COURSE NUMBER: ME 321 Fluid Mechanics I 3 credit hour. Basic Equations in fluid Dynamics

Where does Bernoulli's Equation come from?

where = rate of change of total energy of the system, = rate of heat added to the system, = rate of work done by the system

Generalized Form of the First Law

MECH 5810 Module 3: Conservation of Linear Momentum

Convection Heat Transfer

Detailed Outline, M E 521: Foundations of Fluid Mechanics I

Chapter 2: Basic Governing Equations

Chapter 4: Fluid Kinematics

Objectives. Conservation of mass principle: Mass Equation The Bernoulli equation Conservation of energy principle: Energy equation

Thermodynamics ENGR360-MEP112 LECTURE 7

Chapter 5: Mass, Bernoulli, and

Getting started: CFD notation

ME 300 Thermodynamics II

Chapter 9: Differential Analysis

ROAD MAP... D-0: Reynolds Transport Theorem D-1: Conservation of Mass D-2: Conservation of Momentum D-3: Conservation of Energy

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

Pressure Losses for Fluid Flow Through Abrupt Area. Contraction in Compact Heat Exchangers

2.29 Numerical Fluid Mechanics Fall 2011 Lecture 5

Chapter 5: Mass, Bernoulli, and Energy Equations

Chapter 9: Differential Analysis of Fluid Flow

Detailed Outline, M E 320 Fluid Flow, Spring Semester 2015

Module 2 : Convection. Lecture 12 : Derivation of conservation of energy

MAE 3130: Fluid Mechanics Lecture 7: Differential Analysis/Part 1 Spring Dr. Jason Roney Mechanical and Aerospace Engineering

Watch for typos. This is typed 2003 from handwritten text of Lec. 2.4 Scaling [and exponent relations]

Physical Science and Engineering. Course Information. Course Number: ME 100

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

3.8 The First Law of Thermodynamics and the Energy Equation

Conservation of Momentum using Control Volumes

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

Fluid Dynamics Exercises and questions for the course

Review for Exam Hyunse Yoon, Ph.D. Adjunct Assistant Professor Department of Mechanical Engineering, University of Iowa

Continuum Mechanics Fundamentals

Module 2 : Lecture 1 GOVERNING EQUATIONS OF FLUID MOTION (Fundamental Aspects)

Course Syllabus: Continuum Mechanics - ME 212A

Fluid Mechanics Prof. S. K. Som Department of Mechanical Engineering Indian Institute of Technology, Kharagpur

1. Introduction, tensors, kinematics

AE/ME 339. K. M. Isaac. 9/22/2005 Topic 6 FluidFlowEquations_Introduction. Computational Fluid Dynamics (AE/ME 339) MAEEM Dept.

2 GOVERNING EQUATIONS

2.29 Numerical Fluid Mechanics Fall 2011 Lecture 7

Collisions. Lecture 18. Chapter 11. Physics I. Department of Physics and Applied Physics

Lecture 1: Kinematics, ideal mechanical systems and Bernoulli s equation

(Refer Slide Time: 0:35)

Angular momentum equation

FLOW IN CONDUITS. Shear stress distribution across a pipe section. Chapter 10

Chapter 3. Finite Difference Methods for Hyperbolic Equations Introduction Linear convection 1-D wave equation

Module-3: Kinematics

Last name: First name: Student ID: Discussion: You solution procedure should be legible and complete for full credit (use scratch paper as needed).

A Hamiltonian Numerical Scheme for Large Scale Geophysical Fluid Systems

Section 2: Lecture 1 Integral Form of the Conservation Equations for Compressible Flow

Chapter 8: Flow in Pipes

Computational Fluid Dynamics Prof. Dr. Suman Chakraborty Department of Mechanical Engineering Indian Institute of Technology, Kharagpur

Needs work : define boundary conditions and fluxes before, change slides Useful definitions and conservation equations

Signature: (Note that unsigned exams will be given a score of zero.)

Laplace Transforms Chapter 3

Energy CEEN 598D: Fluid Mechanics for Hydro Systems. Lindsay Bearup Berthoud Hall 121

Introduction to Fluid Machines and Compressible Flow Prof. S. K. Som Department of Mechanical Engineering Indian Institute of Technology, Kharagpur

(Refer Slide Time: 3:39)

Applied Thermodynamics for Marine Systems Prof. P. K. Das Department of Mechanical Engineering Indian Institute of Technology, Kharagpur

Chapter 1. Continuum mechanics review. 1.1 Definitions and nomenclature

Basic Thermodynamics Prof. S.K. Som Department of Mechanical Engineering Indian Institute of Technology, Kharagpur

Lecture Notes #10. The "paradox" of finite strain and preferred orientation pure vs. simple shear

AA210A Fundamentals of Compressible Flow. Chapter 5 -The conservation equations

Performance. 5. More Aerodynamic Considerations

SOE3213/4: CFD Lecture 3

Detailed Derivation of Fanno Flow Relationships

Lecture Note for Open Channel Hydraulics

CLASS SCHEDULE 2013 FALL

Chapter 0. Preliminaries. 0.1 Things you should already know

Lecture 17. Conservation of Linear Momentum

GG303 Lecture 15 10/6/09 1 FINITE STRAIN AND INFINITESIMAL STRAIN

The Second Law of Thermodynamics

Chemical Engineering 693R

in this web service Cambridge University Press

Thermodynamics 1. Lecture 7: Heat transfer Open systems. Bendiks Jan Boersma Thijs Vlugt Theo Woudstra. March 1, 2010.

Acoustic Energy Estimates in Inhomogeneous Moving Media

Damped Harmonic Oscillator

Lecture 16. Conservation of Linear Momentum

Mathematica. 1? Birkhauser. Continuum Mechanics using. Fundamentals, Methods, and Applications. Antonio Romano Addolorata Marasco.

Direct method for deriving equilibrium equations in solid continuous systems

Astrophysical Fluid Dynamics (2)

Lecture 21: Isoparametric Formulation of Plane Elements.

Chapter 7. Three Dimensional Modelling of Buoyancy-Driven Displacement Ventilation: Point Source

AN INTRODUCTION TO LAGRANGE EQUATIONS. Professor J. Kim Vandiver October 28, 2016

Thermodynamic Systems

Introduction to Fluid Machines and Compressible Flow Prof. S. K. Som Department of Mechanical Engineering Indian Institute of Technology, Kharagpur

Analysis of hydrodynamic forces on non-spherical particles (Spherocylinder)

Advanced Hydraulics Prof. Dr. Suresh A. Kartha Department of Civil Engineering Indian Institute of Technology, Guwahati

Transcription:

M E 320 Professor John M. Cimbala Lecture 10 Today, we will: Discuss the Reynolds Transport Theorem (RTT) Show how the RTT applies to the conservation laws Begin Chapter 5 Conservation Laws D. The Reynolds Transport Theorem (RTT) (Section 4-6) 1. Introduction and derivation The Reynolds Transport Theorem (RTT) (Section 4-6) Recall from Thermodynamics: A system [also called a closed system] is a quantity of matter of fixed identity. No mass can cross a system boundary. A control volume [also called an open system] is a region in space chosen for study. Mass can cross a control surface (the surface of the control volume). The fundamental conservation laws (conservation of mass, energy, and momentum) apply directly to systems. However, in most fluid mechanics problems, control volume analysis is preferred over system analysis (for the same reason that the Eulerian description is usually preferred over the Lagrangian description). Therefore, we need to transform the conservation laws from a system to a control volume. This is accomplished with the Reynolds transport theorem (RTT). There is a direct analogy between the transformation from Lagrangian to Eulerian descriptions (for differential analysis using infinitesimally small fluid elements) and the transformation from systems to control volumes (for integral analysis using large, finite flow fields): Differential analysis The material derivative is used to transform from Lagrangian to Eulerian descriptions for differential analysis Integral analysis The Reynolds transport theorem is used to transform from system to control volume for integral analysis FIGURE 4-64 In both cases, the fundamental laws of physics (conservation laws) are known in the analysis on the left (Lagrangian or system), and must be transformed so as to be useful in the analysis on the right (Eulerian or control volume).

Another way to think about the RTT is that it is a link between the system approach and the control volume approach: FIGURE 4-54 See text for detailed derivation of the RTT. Here are some highlights: Let B represent any extensive property (like mass, energy, or momentum). Let b be the corresponding intensive property, i.e., b = B/m (property B per unit mass). Our goal is to find a relationship between B sys or b sys (property of the system, for which we know the conservation laws) and B CV or b CV (property of the control volume, which we prefer to use in our analysis). The results are shown below in various forms: For fixed (non-moving and non-deforming) control volumes, Since the control volume is fixed, the order of integration or differentiation does not matter, i.e. d... dt is the same as CV CV... t equivalent for a fixed control volume.. Thus, the two circled quantities above are

For nonfixed (moving and/or deforming) control volumes, Note that we replace V by r V in this version of the RTT for a moving and/or deforming control volume. where Error! Objects cannot be created from editing field codes. is the relative velocity, i.e., the velocity of the fluid relative to the control surface (which may be moving or deforming), We can also switch the order of the time derivative and the integral in the first term on the right, but only if we use the absolute (rather than the relative) velocity in the second term on the right, i.e., Comparing Eqs. 4-45 and 4-42, we see that they are identical. Thus, the most general form of the RTT that applies to both fixed and non-fixed control volumes is Even though this equation is most general, it is often easier in practice to use Eq. 4-44 for moving and/or deforming (non-fixed) control volumes because the algebra is easier. Simplifications: For steady flow, the volume integral drops out. In terms of relative velocity, For control volumes where there are well-defined inlets and outlets, the control surface integral can be simplified, avoiding cumbersome integrations, Note that the above equation is approximate, and may not always be accurate.