AOE 5104 Class 10 Online presentations for next class: –Potential Flow 1 Homework 4 due 10/2.

Slides:



Advertisements
Similar presentations
Boundary layer with pressure gradient in flow direction.
Advertisements

Lakshmi Sankar Module 3.3 Panel Methods Lakshmi Sankar
Instructor: André Bakker
Lift Theories Linear Motion.
Sources of the Magnetic Field
MECH 221 FLUID MECHANICS (Fall 06/07) Chapter 7: INVISCID FLOWS
Chapter 22 Magnetism AP Physics B Lecture Notes.
Chapter 28. Magnetic Field
Fisica Generale - Alan Giambattista, Betty McCarty Richardson Copyright © 2008 – The McGraw-Hill Companies s.r.l. 1 Chapter 19: Magnetic Forces and Fields.
Conservation of Linear Momentum.
W11D2 Concept Questions Review
Boundary Layer Flow Describes the transport phenomena near the surface for the case of fluid flowing past a solid object.
Fisica Generale - Alan Giambattista, Betty McCarty Richardson Copyright © 2008 – The McGraw-Hill Companies s.r.l. 1 Chapter 16: Electric Forces and Fields.
Flow over immersed bodies. Boundary layer. Analysis of inviscid flow.
External Flows.
Fall 2008Physics 231Lecture 7-1 Magnetic Forces. Fall 2008Physics 231Lecture 7-2 Magnetic Forces Charged particles experience an electric force when in.
Atmospheric Motion ENVI 1400: Lecture 3.
Chapter 9 Solids and Fluids (c).
17 VECTOR CALCULUS.
D A C B z = 20m z=4m Homework Problem A cylindrical vessel of height H = 20 m is filled with water of density to a height of 4m. What is the pressure at:
AOSS 321, Winter 2009 Earth System Dynamics Lecture 6 & 7 1/27/2009 1/29/2009 Christiane Jablonowski Eric Hetland
Momentum flux across the sea surface
MECH 221 FLUID MECHANICS (Fall 06/07) Chapter 4: FLUID KINETMATICS
Physics 121: Electricity & Magnetism – Lecture 9 Magnetic Fields Dale E. Gary Wenda Cao NJIT Physics Department.
Forces Acting on a Control Volume Body forces: Act through the entire body of the control volume: gravity, electric, and magnetic forces. Surface forces:
Fluid mechanics 3.1 – key points
LAMINAR PLANE COUETTE AND OPEN CHANNEL FLOW
AOE 5104 Class 4 9/4/08 Online presentations for today’s class: –Vector Algebra and Calculus 2 and 3 Vector Algebra and Calculus Crib Homework 1 Homework.
Hans Burchard Leibniz Institute for Baltic Sea Research Warnemünde Coastal Ocean Dynamics First course: Hydrodynamics.
ELECTRICITY & MAGNETISM (Fall 2011) LECTURE # 4 BY MOEEN GHIYAS.
The Air-Sea Momentum Exchange R.W. Stewart; 1973 Dahai Jeong - AMP.
Momentum. NEWTON’S LAWS Newton’s laws are relations between motions of bodies and the forces acting on them. –First law: a body at rest remains at rest,
Drag Lecture 6 Chapter 3.
6 Life in a Fluid Medium. CONSIDER FLUID MOVING IN STREAMLINES: Water flow can be visualized as streamlines Particles entrained in flow move with streamlines.
Ch 9: Part B – Fluid Flow About Immersed Bodies Flow Stream U Drag = pressure + friction.
Introduction to Fluid Mechanics
AOE 5104 Class 9 Online presentations for next class:
Kinematics of Flow. Fluid Kinematics  Fluid motion -Types of fluid - Velocity and acceleration - Continuity equation  Potential Flows -Velocity Potential.
KINEMATICS Kinematics describes fluid flow without analyzing the forces responsibly for flow generation. Thereby it doesn’t matter what kind of liquid.
Momentum Equations in a Fluid (PD) Pressure difference (Co) Coriolis Force (Fr) Friction Total Force acting on a body = mass times its acceleration (W)
Mass Transfer Coefficient
Chapter 4 FLOWING FLUIDS AND PRESSURE VARIATION Fluid Mechanics Source:
Reynolds Transport Theorem We need to relate time derivative of a property of a system to rate of change of that property within a certain region (C.V.)
CEE 262A H YDRODYNAMICS Lecture 15 Unsteady solutions to the Navier-Stokes equation.
FLUID Characteristics of Fluid Flow (1) Steady flow (lamina flow, streamline flow) The fluid velocity (both magnitude and direction) at any given point.
1 WHAT IS A BOUNDARY LAYER? A boundary layer is a layer of flowing fluid near a boundary where viscosity keeps the flow velocity close to that of the boundary.
AOE 5104 Class 8 Online presentations for next class: –Kinematics 2 and 3 Homework 3 (thank you) Homework 4 (6 questions, 2 graded, 2 recitations, worth.
Lecture 7: Unsteady Laminar Flow
Panel methods to Innovate a Turbine Blade-1 P M V Subbarao Professor Mechanical Engineering Department A Linear Mathematics for Invention of Blade Shape…..
Atmospheric Motion SOEE1400: Lecture 7. Plan of lecture 1.Forces on the air 2.Pressure gradient force 3.Coriolis force 4.Geostrophic wind 5.Effects of.
Pharos University MECH 253 FLUID MECHANICS II
The Laws of Motion Newton’s Three Laws of Motion:
Ch 4 Fluids in Motion.
OC FLOW: ENERGY CONCEPTS, CHANNEL ANALYSIS
MECH 221 FLUID MECHANICS (Fall 06/07) Chapter 8: BOUNDARY LAYER FLOWS
Electric Field.
THE BOUNDARY LAYER: AN INTRODUCTION  In a flow, the boundary layer represents a (relatively) thin layer of fluid that is nearest the solid boundary
VII. Analysis of Potential Flows. Contents 1. Preservation of Irrotationality 2. Description of 2D Potential Flows 3. Fundamental Solutions 4. Superposition.
NNPC FSTP ENGINEERS Physics Course Code: Lesson 7.
Physics. Session Fluid Mechanics - 2 Session Objectives.
Flowing Fluids ( 유체의 흐름 ) Fluid kinematics ( 유체운동학 ) – describes the motion of fluid elements such as translation ( 이동 ), transformation ( 변형 ), rotation.
External flow: drag and Lift
Advanced Dynamical Meteorology Roger K. Smith CH 05.
Nighttime exam? If we have the exam in the evening of July 3 rd, we would cancel class on July 5 th and you get a long weekend. Would you prefer to have.
Electric Field & Magnetic Field
CE 3305 Engineering FLUID MECHANICS
King Saud university Norah Ali Al-Moneef
Fluid Mechanics & Hydraulics
Subject Name: FLUID MECHANICS
Electric Field Lines Drawing electric field lines
Presentation transcript:

AOE 5104 Class 10 Online presentations for next class: –Potential Flow 1 Homework 4 due 10/2

Kinematics of Vorticity

Kinematic Concepts - Vorticity Boundary layer growing on flat plate Cylinder projecting from plate Vortex Line: A line everywhere tangent to the vorticity vector. Vortex lines may not cross. Rarely are they streamlines. Thread together axes of spin of fluid particles. Given by ds  =0. Could be a fluid line? Vortex sheet: Surface formed by all the vortex lines passing through the same curve in space. No vorticity flux through a vortex sheet, i.e. .ndS=0 Vortex tube: Vortex sheet rolled so as to form a tube. n dS  Vortex line Vortex tube Vortex sheet

Spiral vortices formed on a 20cm-wide spinning cone at 2.9m/s. Boundary layer is revealed. Spinning Cone

Implications (Helmholtz’ Vortex Theorems, Part 1) The strength of a vortex tube (defined as the circulation around it) is constant along the tube. The tube, and the vortex lines from which it is composed, can therefore never end. They must extend to infinity or form loops. The average vorticity magnitude inside a vortex tube is inversely proportional to the cross- sectional area of the tube

Vortex Tube Section 1 Section 2 n dS Since So, we call  The Vortex Tube Strength

Implications (Helmholtz’ Vortex Theorems, Part 1) The strength of a vortex tube (defined as the circulation around it) is constant along the tube. The tube, and the vortex lines from which it is composed, can therefore never end. They must extend to infinity or form loops. The average vorticity magnitude inside a vortex tube is inversely proportional to the cross- sectional area of the tube

Kinematic Concepts - Vorticity Boundary layer growing on flat plate Cylinder projecting from plate Vortex Line: A line everywhere tangent to the vorticity vector. Vortex lines may not cross. Rarely are they streamlines. Thread together axes of spin of fluid particles. Given by ds  =0. Could be a fluid line? Vortex sheet: Surface formed by all the vortex lines passing through the same curve in space. No vorticity flux through a vortex sheet, i.e. .ndS=0 Vortex tube: Vortex sheet rolled so as to form a tube. n dS  Vortex line Vortex tube Vortex sheet

But, does the vortex tube travel along with the fluid, or does it have a life of it’s own? Fluid loop C at time t Same fluid loop at time t+dt Vdt (V+dV)dt If it moves with the fluid, then the circulation around the fluid loop shown should stay the same. ds 0

Fluid loop at time t Same fluid loop at time t+dt Vdt (V+dV)dt So the rate of change of  around the fluid loop is Now, the momentum eq. tell us that Body force per unit mass Pressure force per unit mass Viscous force per unit mass, say f v ‘Body force torque’ ‘Pressure force torque’ Viscous force ‘torque’ So, in general

Body Force Torque Stokes Theorem For gravity So, body force torque is zero for gravity and for any irrotational body force field Therefore, body force torque is zero for most practical situations

Pressure Force Torque If density is constant So, pressure force torque is zero. Also true as long as  =  (p). Pressure torques generated by Curved shocks Free surface / stratification

Shock in a CD Nozzle Bourgoing & Benay (2005), ONERA, France Schlieren visualization Sensitive to in-plane index of ref. gradient

Viscous Force Torque Viscous force torques are non-zero where viscous forces are present ( e.g. Boundary layer, wakes) Can be really small, even in viscous regions at high Reynolds numbers since viscous force is small in that case The viscous force torques can then often be ignored over short time periods or distances

Shock in a CD Nozzle Bourgoing & Benay (2005), ONERA, France Schlieren visualization Sensitive to in-plane index of ref. gradient

Implications In the absence of body-force torques, pressure torques and viscous torques… the circulation around a fluid loop stays constant: Kelvin’s Circulation Theorem a vortex tube travels with the fluid material (as though it were part of it), or –a vortex line will remain coincident with the same fluid line –the vorticity convects with the fluid material, and doesn’t diffuse –fluid with vorticity will always have it –fluid that has no vorticity will never get it ‘Body force torque’ ‘Pressure force torque’ Viscous force ‘torque’ Helmholtz’ Vortex Theorems, Part 2

Lord Kelvin ( ) (William Thompson )

Vorticity Transport Equation The kinematic condition for convection of vortex lines with fluid lines is found as follows After a lot of math we get....

Example: Irrotational Flow? Consider a vehicle moving at constant speed in homogeneous medium (i.e. no free surfaces) under the action of gravity, moving into a stationary fluid. Apparent uniform flow (V = const.) Far ahead of the sub we have that (since V = const.) and the flow here is irrotational. Now, the flow generates no body force or pressure torques and, except in the vehicle boundary layer and wake, no viscous torques. So, the flow will remain irrotational everywhere outside the boundary layer and wake, regardless of how complex we make the sub shape.

Example: The Starting Vortex Consider a stationary arifoil in a stationary medium. L  V = 0 V = const. Now suppose the airfoil starts moving to left. (Using the fact that that a lifting airfoil in motion has a circulation about it). Fluid loop C  C remains 0 by Kelvin´s Theorem, if the loop remains outside the airfoil wake, Thus a vortex of circulation equal and opposite to that on the airfoil must be shed. -- Starting vortex

Starting Vortex Pictures are from “An Album of Fluid Motion” by Van Dyke

Example: Flow over a depression in a river bed A river flows over a depression locally doubling the depth. The river contains turbulence that is too weak to change the overall flow pattern. An turbulent eddy convects from upstream over the depression. Estimate its strength in the depression if the eddy is initially (a) vertical, and (b) horizontal. h 2h Solution: Need to assume that the viscous torques are not significant for the eddy so that the fluid tube it occupies remains coincident with the same fluid tube. (a)The vertical fluid tube occupied by the eddy will double in length in the depression and so (by continuity) it will halve its cross sectional area. By Helmholtz’ theorems, halving the cross sectional area of a vortex tube will double the vorticity. Hence  2 =2  1 in this case. (b) The horizontal fluid tube containing the eddy will double its height and halve its length as it goes over the depression. Its cross-sectional area will thus double and by Helmhotz’ theorems the vorticity will halve. Hence  2 = ½  1 in this case.

The River Avon nearing flood stage, Salisbury, Wiltshire, UK

Example: Evolution of turbulence in a shear flow Turbulence is convected and distorted in a shear flow, as shown. Consider an eddy that at time t=0 is vertically aligned and has a vorticity  o. Estimate the vorticity magnitude and angle of an eddy, as functions of time. Solution: Need to assume that the viscous torques are not significant for the eddy so that the fluid tube it occupies remains coincident with the same fluid tube. Also need too assume that the eddy is to weak to influence the flow that is convecting it. U=ky, k=const y y l klt Time 0 Time t Consider a segment of the eddy of length l. In time t the top of the eddy will convect further than the bottom by an amount equal to the difference in the velocity ( kl ) times the time. The angle of the fluid tube containing the eddy will thus be The fluid tube also grows longer by the factor The cross sectional area of the tube thus reduces by this factor, and therefore the vorticity increases by this factor, i.e.

Eddies in a turbulent channel flow DNS Simulation Thomas Bewley, Edward Hammond & Parviz Moin Stanford University

Example: Flow around a corner in a channel Air flows through a duct with a 6 o corner. An initially vertical eddy is introduced into the otherwise uniform flow upstream and convects around the corner. Estimate its orientation downstream. Solution: Need to assume that the viscous torques are not significant for the eddy so that the fluid tube it occupies remains coincident with the same fluid tube, and so that no vorticity is generated in the turn. Also need to assume that the eddy is too weak to influence the flow that is convecting it. Consider two initially perpendicular fluid lines, one in the streamwise direction and one vertical, coincident with the eddy. Since there is no vorticity component perpendicular to the page, and no torques to generate any, the sum of the rotation rates of these two fluid lines must remain zero. The streamwise fluid line will follow the streamline and thus rotate counterclockwise by 6 o. The vertical fluid line and thus the eddy must therefore rotate clockwise by 6 o, as shown. 6o6o 6o6o 6o6o

Turbulent flow in a pipe through a 180 o bend. Hitoshi Sugiyama, Utsunomiya University

Ox Bows