V 1. Conservation of Mass dz dy dx

Slides:



Advertisements
Similar presentations
Differential Calculus (revisited):
Advertisements

Conservation of Linear Momentum.
The Ultimate Importance of Invariant Property : Rothalpy
Quiz 2 –
Chapter 2 Reynolds Transport Theorem (RTT) 2.1 The Reynolds Transport Theorem 2.2 Continuity Equation 2.3 The Linear Momentum Equation 2.4 Conservation.
Lecture 8: Div(ergence) S Consider vector field and Flux (c.f. fluid flow of Lecture 6) of out of S rate of flow of material (in kg s -1 ) out of S For.
Conservation Vector Review Mass Balance General Statement Simplifications The Control Volume A Useable Form Problems.
2-1 Problem Solving 1. Physics  2. Approach methods
1 MAE 5130: VISCOUS FLOWS Momentum Equation: The Navier-Stokes Equations, Part 1 September 7, 2010 Mechanical and Aerospace Engineering Department Florida.
Fluids. Eulerian View  In a Lagrangian view each body is described at each point in space. Difficult for a fluid with many particles.  In an Eulerian.
Numerical Hydraulics Wolfgang Kinzelbach with Marc Wolf and Cornel Beffa Lecture 1: The equations.
Instructor: André Bakker
Module 3 Fluid Flow. Lesson 20 CONTINUITY EQUATION DESCRIBE how the density of a fluid varies with temperature. DEFINE the term buoyancy. DESCRIBE the.
General Formulation - A Turbojet Engine
ME 231 Thermofluid Mechanics I Navier-Stokes Equations.
1 April 14 Triple product 6.3 Triple products Triple scalar product: Chapter 6 Vector Analysis A B C + _.
R. Field 10/29/2013 University of Florida PHY 2053Page 1 Ideal Fluids in Motion Bernoulli’s Equation: The Equation of Continuity: Steady Flow, Incompressible.
Conservation of Mass D=Domain of a body of water Water is flowing in and out of D Mass is neither created nor destroyed Flow coming in = Flow going out.
Chapter 9: Differential Analysis of Fluid Flow SCHOOL OF BIOPROCESS ENGINEERING, UNIVERSITI MALAYSIA PERLIS.
Introduction to Fluid Mechanics
Louisiana Tech University Ruston, LA Momentum Balance Steven A. Jones BIEN 501/CMEN 513 Monday, March 19, 2007.
CHAPTER (III) KINEMATICS OF FLUID FLOW 3.1: Types of Fluid Flow : Real - or - Ideal fluid : Laminar - or - Turbulent Flows : Steady -
Kinematics of Flow. Fluid Kinematics  Fluid motion -Types of fluid - Velocity and acceleration - Continuity equation  Potential Flows -Velocity Potential.
Energy momentum tensor of macroscopic bodies Section 35.
ME 254. Chapter I Integral Relations for a Control Volume An engineering science like fluid dynamics rests on foundations comprising both theory and experiment.
1 MAE 5130: VISCOUS FLOWS Conservation of Mass September 2, 2010 Mechanical and Aerospace Engineering Department Florida Institute of Technology D. R.
States of matter Solid: Liquid Gas Plasma Fluid: Crystalline Amorphous.
1 MECH 221 FLUID MECHANICS (Fall 06/07) Tutorial 5.
CE 1501 CE 150 Fluid Mechanics G.A. Kallio Dept. of Mechanical Engineering, Mechatronic Engineering & Manufacturing Technology California State University,
Dr. Jason Roney Mechanical and Aerospace Engineering
MAE 5360: Hypersonic Airbreathing Engines
Differential Analysis of Fluid Flow. Navier-Stokes equations Example: incompressible Navier-Stokes equations.
Also known as Gauss’ Theorem
Electricity and Magnetism
Four dimensional current vector Section 28. For convenience, we often consider a distribution of point charges to be a continuous distribution of charge.
Fluid Mechanics (C.V. analysis) Dept. of Experimental Orthopaedics and Biomechanics Bioengineering Reza Abedian (M.Sc.)
Remark: foils with „black background“ could be skipped, they are aimed to the more advanced courses Rudolf Žitný, Ústav procesní a zpracovatelské techniky.
Computer Animation Rick Parent Computer Animation Algorithms and Techniques Computational Fluid Dynamics.
Heat and Flow Technology I.
First Law of Thermodynamics applied to Flow processes
Chapter 6 Vector Analysis
Continuum Mechanics (MTH487)
Continuity Equation.
FLUID MECHANICS LECTURE
MAE 5350: Gas Turbines Integral Forms of Mass and Momentum Equations
MASS AND ENERGY ANALYSIS OF CONTROL VOLUMES
Chapter 9: Differential Analysis of Fluid Flow
Mass and Energy Analysis of Control Volumes
GLOBAL CONSERVATION EQUATIONS
Force acting on a charged particle moving through a magnetic field
GLOBAL CONSERVATION EQUATIONS
Introduction to Fluid Mechanics
Continuum Mechanics for Hillslopes: Part IV
AE/ME 339 Computational Fluid Dynamics (CFD) K. M. Isaac 11/15/2018
INFINITESIMALLY SMALL DIFFERENTIAL CUBE IN SPACE
THERMO- AND FLUID MECHANICS LECTURE
MAE 4261: AIR-BREATHING ENGINES
Chapter 6 Vector Analysis
Topic 6 FluidFlowEquations_Introduction
MASS AND VOLUMETRIC FLOWRATES
AE/ME 339 Computational Fluid Dynamics (CFD) K. M. Isaac 12/3/2018
MAE 4262: Rockets and Mission Analysis
Today’s Lecture Objectives:
Fluid Theory: Magnetohydrodynamics (MHD)
MAE 3241: AERODYNAMICS AND FLIGHT MECHANICS
Topic 6 NavierStokes Equations
The mass conservation implies that the same amount of water flows through the narrow and large tubes. In particular the same mass of water enters and leaves.
5. Describing Flow CH EN 374: Fluid Mechanics.
Richard B. Rood (Room 2525, SRB) University of Michigan
Ch. 4 The first law of thermodynamics: Control Volume
Presentation transcript:

V 1. Conservation of Mass dz dy dx A continuous fluid can be thought of as being made up of a large group of elemental fluid particles. These particles jostle along shoulder to shoulder as the fluid moves.

V 2. Fluid Particle dz dy dx Each particle moves at a velocity (V) and has a volume (dx, dy, dz) and density (). Each has an individual mass ( m= .dx.dy.dz).

3. Conservation of Particle Mass When moving with the flow, particles may be distorted (stretched, compressed, sheared or rotated) due to the pressure and temperature fields that they pass through. However their individual masses remain unchanged.

4. Control Volume  For the control volume (), the mass contained within will be the sum of the masses of all the fluid particles.

5. Flow through Control Volume If the fluid is moving, then all fluid particles can be tracked over a small period of time (t). Particle mass will be conserved. The change in fluid mass in the volume will equal the difference in mass of particles entering compared to mass of particles leaving.

Outflow V (t) C Inflow B 6. Inflow and Outflow This can be written as Mass Change in Volume () = Inflow (B) –Outflow mass(C) Outflow V (t) C Inflow B

In limit as t 0 7. Equations of Mass Flow Mass Change in Volume () = Inflow (B) –Outflow mass(C) In limit as t 0

-Vn dl V dA B  n 8. Inflow Rate The amount of mass entering the control volume through an elemental surface, area dA, can be calculated using the component of velocity normal to the surface -Vn dl V Thus incoming flow rate is dA B  n

Vn  V dl dA C 9. Outflow Rate The amount of mass exiting the control volume through surface, dA, can also be calculated using the component of velocity normal to this surface Vn  V dl Thus the flow rate through the exit surface is dA C

10. Integral Equation Form Substituting for the incoming and outgoing flow rates in the mass conservation balance for volume () leads to the result, Integral Form