Problem 1 1- To verify whether the flow satisfies conservation of mass, we consider the continuity
|
|
- Mildred Jones
- 5 years ago
- Views:
Transcription
1 Problem 1 1- To verif whether the flow satisfies conservation of mass, we consider the continuit u v equation for D incompressible flow: 0 x u x x x 1 x 1 x v x 1 x 1 Therefore: u v 1 x x1 0, x which demonstrates that conservation of mass is satisfied. - Matlab code: %plot velocit vector field clear all; %create the matrices containing the x and coordinates of all points in the domain [X,Y]=meshgrid(-10:1:10, -10:1:10); r=size(x,1); c=size(x,); %at each point, calculate the x- and -components of the velocit for i=1:r for j=1:c U(i,j)=Y(i,j)^-X(i,j)*(1+X(i,j)); V(i,j)=Y(i,j)*(*X(i,j)+1); %plot the vector field over the domain quiver(x,y,u,v) axis square xlabel('x'); label('y');
2 Plot: 3- The components of the acceleration vector can be obtained b taking the material derivative of the velocit components: Similarl: Du u u ax V u u v u Dt t t x Dv v v a V v u v v Dt t t x u u u t x t x a x u v x x u x x v x x 0 1 x a 1 x x1 x x 1 x 1 x1 x x a x 1 u x 1 v x 1 t x 0 x1
3 a x 1 x x 1 Therefore, the acceleration field is defined as: In particular, at point 1,1 : 1 1 ax x x x a x 1 x x 1 ax 1,1 9 a a 1,1 7 1, m/s Problem 1- One velocit component, the other is unknown. The continuit equation can be used to determine the unknown velocit component. For an incompressible flow: u v 0 x u Since u x, x and substituting this in the continuit equation ields: v Integrating both sides with respect to : v( x, ) f ( x) In order to determine the unknown function f( x ), we consider the boundar condition provided in the problem (i.e., along the x-axis, the -component of the velocit is zero). Translated mathematicall: Using the expression derived for v( x, ) : v 0 at f( x) f( x) 0 Therefore, the unknown velocit component is: v( x, )
4 - Matlab code: %plot velocit vector field clear all; %create the matrices containing the x and coordinates of all points in the domain [X,Y]=meshgrid(0:1:10, 0:1:10); r=size(x,1); c=size(x,); %at each point, calculate the x- and -components of the velocit for i=1:r for j=1:c U(i,j)=*X(i,j); V(i,j)=-*Y(i,j); %plot the vector field over the domain quiver(x,y,u,v) axis square xlabel('x'); label('y'); Plot: S3- The volumetric flow rate (per unit depth of the page) q across the line AB is related to the average velocit V of the fluid across that line b the following relationship:
5 where L is the length of the line AB. q VL, q is obtained b taking the difference in the value of the streamfunction between point A and point B (see streamfunction properties): q (1,1) (0,0). Therefore: (1,1) (0,0) V L Let s determine the streamfunction expression: u x v x Integrating the 1 st relationship with respect to : ( x, ) x f ( x) Substituting this result in the second relationship: ( x f ( x)) x x f ( x) f( x) 0 f ( x) C We obtained the final form of the streamfunction: ( x, ) x C The constant C to zero: does not serve an purpose in this expression and can therefore be set equal Using this expression: Substituting in the velocit expression: ( x, ) x (0, 0) 0 (1,1) Quantitativel: V 1.41 m/s V L
6 Problem 3 1- A stagnation point is a point where the velocit is zero. It can be found b solving the sstem of equations: u 0 v x x There is one single stagnation point. - Matlab code: %plot velocit vector field clear all; %create the matrices containing the x and coordinates of all points in the domain [X,Y]=meshgrid(-:0.:, 0:0.5:5); r=size(x,1); c=size(x,); %at each point, calculate the x- and -components of the velocit for i=1:r for j=1:c U(i,j)= *X(i,j); V(i,j)= *Y(i,j); %plot the vector field over the domain quiver(x,y,u,v) axis square xlabel('x'); label('y'); hold on; %plot streamline passing through (1,) X=-:0.05:; Y=zeros(1,length(X)); for i=1:length(x) Y(1,i)=(1.5/0.8)-(1.3*0.7)/(0.8*( *X(i))); plot(x,y); axis([- 0 5]); Plot:
7 3- Acceleration field: ˆ ˆ u v u v u ˆ v ˆ DV V a V V i j i j Dt t t x ˆ ˆ a x x x ˆ ˆ t i j x i j a x x ˆ ˆ x ˆ x ˆ i j i j x0.8 ˆ i ˆj a xˆi a ax a 4- Streamline equation The first step is to establish the streamfunction expression. We start with: ˆj
8 u x Integrating on both sides with respect to : x f ( x) Using this intermediate result, the other relationship v x can be written: x Substituting in the intermediate result ields: x f ( x) f ( x) f( x) 1.5 f ( x) 1.5x C x 1.5x C Since the constant C to zero: does not pla an role in the streamfunction, it can be set arbitraril equal x 1.5x The streamline equation is obtained b setting the streamfunction equal to a constant (i.e., A): x 1.5x A A1.5x x
CHAPTER 3 Introduction to Fluids in Motion
CHAPTER 3 Introduction to Fluids in Motion FE-tpe Eam Review Problems: Problems 3- to 3-9 nˆ 0 ( n ˆi+ n ˆj) (3ˆi 4 ˆj) 0 or 3n 4n 0 3. (D) 3. (C) 3.3 (D) 3.4 (C) 3.5 (B) 3.6 (C) Also n n n + since ˆn
More informationBoundary-Fitted Coordinates!
Computational Fluid Dnamics http:wwwndedu~gtrggvacfdcourse Computational Fluid Dnamics Computational Methods or Domains with Comple BoundariesI Grétar Trggvason Spring For most engineering problems it
More informationOUTLINE FOR Chapter 3
013/4/ OUTLINE FOR Chapter 3 AERODYNAMICS (W-1-1 BERNOULLI S EQUATION & integration BERNOULLI S EQUATION AERODYNAMICS (W-1-1 013/4/ BERNOULLI S EQUATION FOR AN IRROTATION FLOW AERODYNAMICS (W-1-.1 VENTURI
More informationChapter 4. Motion in Two Dimensions. Professor Wa el Salah
Chapter 4 Motion in Two Dimensions Kinematics in Two Dimensions Will study the vector nature of position, velocity and acceleration in greater detail. Will treat projectile motion and uniform circular
More informationMethod of Images
. - Marine Hdrodnamics, Spring 5 Lecture 11. - Marine Hdrodnamics Lecture 11 3.11 - Method of Images m Potential for single source: φ = ln + π m ( ) Potential for source near a wall: φ = m ln +( ) +ln
More informationHalliday/Resnick/Walker 7e Chapter 4
HRW 7e Chapter 4 Page of Hallida/Resnick/Walker 7e Chapter 4 3. The initial position vector r o satisfies r r = r, which results in o o r = r r = (3.j ˆ 4.k) ˆ (.i ˆ 3.j ˆ + 6. k) ˆ =.ˆi + 6.ˆj k ˆ where
More informationConservation of Linear Momentum
Conservation of Linear Momentum Once we have determined the continuit equation in di erential form we proceed to derive the momentum equation in di erential form. We start b writing the integral form of
More informationModule 1 : The equation of continuity. Lecture 4: Fourier s Law of Heat Conduction
1 Module 1 : The equation of continuit Lecture 4: Fourier s Law of Heat Conduction NPTEL, IIT Kharagpur, Prof. Saikat Chakrabort, Department of Chemical Engineering Fourier s Law of Heat Conduction According
More informationVISUAL PHYSICS ONLINE KINEMATICS DESCRIBING MOTION
VISUAL PHYSICS ONLINE KINEMATICS DESCRIBING MOTION The language used to describe motion is called kinematics. Surprisingl, ver few words are needed to full the describe the motion of a Sstem. Warning:
More informationAE/ME 339. K. M. Isaac Professor of Aerospace Engineering. December 21, 2001 topic13_grid_generation 1
AE/ME 339 Professor of Aerospace Engineering December 21, 2001 topic13_grid_generation 1 The basic idea behind grid generation is the creation of the transformation laws between the phsical space and the
More informationComputational Fluid Dynamics (CFD, CHD)*
1 / 1 Computational Fluid Dnamics (CFD, CHD)* PDE (Shocks 1st); Part I: Basics, Part II: Vorticit Fields Rubin H Landau Sall Haerer, Producer-Director Based on A Surve of Computational Phsics b Landau,
More informationReview of the Fundamentals of Groundwater Flow
Review of te Fundamentals of Groundwater Flow Darc s Law 1 A 1 L A or L 1 datum L : volumetric flow rate [L 3 T -1 ] 1 : draulic ead upstream [L] A : draulic ead downstream [L] : draulic conductivit [L
More informationLECTURE NOTES - III. Prof. Dr. Atıl BULU
LECTURE NOTES - III «FLUID MECHANICS» Istanbul Technical University College of Civil Engineering Civil Engineering Department Hydraulics Division CHAPTER KINEMATICS OF FLUIDS.. FLUID IN MOTION Fluid motion
More informationME 3560 Fluid Mechanics
ME 3560 Fluid Mechanics 1 4.1 The Velocity Field One of the most important parameters that need to be monitored when a fluid is flowing is the velocity. In general the flow parameters are described in
More informationConservation of Linear Momentum for a Differential Control Volume
Conservation of Linear Momentum for a Differential Control Volume When we applied the rate-form of the conservation of mass equation to a differential control volume (open sstem in Cartesian coordinates,
More informationFLUIDS Problem Set #3 SOLUTIONS 10/27/ v y = A A = 0. + w z. Y = C / x
FLUIDS 2009 Problem Set #3 SOLUTIONS 10/27/2009 1.i. The flow is clearly incompressible because iu = u x + v y + w z = A A = 0 1.ii. The equation for a streamline is dy dx = Y. Guessing a solution of the
More informationFluid Mechanics II. Newton s second law applied to a control volume
Fluid Mechanics II Stead flow momentum equation Newton s second law applied to a control volume Fluids, either in a static or dnamic motion state, impose forces on immersed bodies and confining boundaries.
More informationChapter 4. Motion in Two Dimensions
Chapter 4 Motion in Two Dimensions Kinematics in Two Dimensions Will study the vector nature of position, velocity and acceleration in greater detail Will treat projectile motion and uniform circular motion
More informationTutorial 6. Fluid Kinematics
Tutorial 6 Fluid Kinematics 1. Water is flowing through a pipe of 2.5cm diameter with a velocity of 0.5m/s. Compute the discharge in m 3 /s and litres/s. Diameter of pipe (d) = 2.5cm = 0.025m C/S Area
More information8.7 Systems of Non-Linear Equations and Inequalities
8.7 Sstems of Non-Linear Equations and Inequalities 67 8.7 Sstems of Non-Linear Equations and Inequalities In this section, we stud sstems of non-linear equations and inequalities. Unlike the sstems of
More informationSeveral Examples on Solving an ODE using MATALB
Several Examples on Solving an ODE using MATALB Introduction: A Tutorial on Solving an ODE through the use of the discretization method then using the MATLAB ODE solver and comparing the results. Two examples
More informationChapter 2 Radical Functions Assignment
Chapter Radical Functions Assignment Name: Short Answer 1. Determine the equation of each radical function, which has been transformed from b the given translations. a) vertical stretch b a factor of 5,
More informationAE301 Aerodynamics I UNIT B: Theory of Aerodynamics
AE301 Aerodynamics I UNIT B: Theory of Aerodynamics ROAD MAP... B-1: Mathematics for Aerodynamics B-: Flow Field Representations B-3: Potential Flow Analysis B-4: Applications of Potential Flow Analysis
More informationMath 181/281. Rumbos Spring 2011 Page 1. Solutions to Assignment #5. Hence, the dynamical system, θ(t, p, q), for (t, p, q) R 3 corresponding = F.
Math 181/281. Rumbos Spring 2011 Page 1 Solutions to Assignment #5 1. For real numbers a and b with a 2 + b 2 = 0, let F : R 2 R 2 be given b ( ) ( ) ( ) x ax b x F =, for all R 2. (1) bx + a (a) Explain
More informationChapter 2 Basic Conservation Equations for Laminar Convection
Chapter Basic Conservation Equations for Laminar Convection Abstract In this chapter, the basic conservation equations related to laminar fluid flow conservation equations are introduced. On this basis,
More informationENGI Gradient, Divergence, Curl Page 5.01
ENGI 940 5.0 - Gradient, Divergence, Curl Page 5.0 5. e Gradient Operator A brief review is provided ere for te gradient operator in bot Cartesian and ortogonal non-cartesian coordinate systems. Sections
More informationCourse Requirements. Course Mechanics. Projects & Exams. Homework. Week 1. Introduction. Fast Multipole Methods: Fundamentals & Applications
Week 1. Introduction. Fast Multipole Methods: Fundamentals & Applications Ramani Duraiswami Nail A. Gumerov What are multipole methods and what is this course about. Problems from phsics, mathematics,
More informationENGI Gradient, Divergence, Curl Page 5.01
ENGI 94 5. - Gradient, Divergence, Curl Page 5. 5. The Gradient Operator A brief review is provided here for the gradient operator in both Cartesian and orthogonal non-cartesian coordinate systems. Sections
More informationMultiple Integrals. Chapter 4. Section 7. Department of Mathematics, Kookmin Univerisity. Numerical Methods.
4.7.1 Multiple Integrals Chapter 4 Section 7 4.7.2 Double Integral R f ( x, y) da 4.7.3 Double Integral Apply Simpson s rule twice R [ a, b] [ c, d] a x, x,..., x b, c y, y,..., y d 0 1 n 0 1 h ( b a)
More informationApply mass and momentum conservation to a differential control volume. Simple classical solutions of NS equations
Module 5: Navier-Stokes Equations: Appl mass and momentum conservation to a differential control volume Derive the Navier-Stokes equations Simple classical solutions of NS equations Use dimensional analsis
More informationOffshore Hydromechanics
Offshore Hydromechanics Module 1 : Hydrostatics Constant Flows Surface Waves OE4620 Offshore Hydromechanics Ir. W.E. de Vries Offshore Engineering Today First hour: Schedule for remainder of hydromechanics
More informationProject 6.2 Phase Plane Portraits of Almost Linear Systems
Project 6.2 Phase Plane Portraits of Almost Linear Sstems Interesting and complicated phase portraits often result from simple nonlinear perturbations of linear sstems. For instance, the figure below shows
More informationENGI 4430 Advanced Calculus for Engineering Faculty of Engineering and Applied Science Problem Set 3 Solutions [Multiple Integration; Lines of Force]
ENGI 44 Advanced Calculus for Engineering Facult of Engineering and Applied Science Problem Set Solutions [Multiple Integration; Lines of Force]. Evaluate D da over the triangular region D that is bounded
More informationModels 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 informationQ2. The velocity field in a fluid flow is given by
Kinematics of Flid Q. Choose the correct anser (i) streamline is a line (a) hich is along the path of a particle (b) dran normal to the elocit ector at an point (c) sch that the streamlines diide the passage
More informationESCI 485 Air/sea Interaction Lesson 5 Oceanic Boundary Layer
ESCI 485 Air/sea Interaction Lesson 5 Oceanic Boundar Laer References: Descriptive Phsical Oceanograph, Pickard and Emer Introductor Dnamical Oceanograph, Pond and Pickard Principles of Ocean Phsics, Apel
More information1.3 LIMITS AT INFINITY; END BEHAVIOR OF A FUNCTION
. Limits at Infinit; End Behavior of a Function 89. LIMITS AT INFINITY; END BEHAVIOR OF A FUNCTION Up to now we have been concerned with its that describe the behavior of a function f) as approaches some
More information1 are perpendicular to each other then, find. Q06. If the lines x 1 z 3 and x 2 y 5 z
Useful for CBSE Board Examination of Math (XII) for 6 For more stuffs on Maths, please visit : www.theopgupta.com Time Allowed : 8 Minutes Max. Marks : SECTION A 3 Q. Evaluate : sin cos 5. Q. State the
More informationMath Review 1: Vectors
Math Review 1: Vectors Coordinate System Coordinate system: used to describe the position of a point in space and consists of 1. An origin as the reference point 2. A set of coordinate axes with scales
More informationCONSERVATION LAWS AND CONSERVED QUANTITIES FOR LAMINAR RADIAL JETS WITH SWIRL
Mathematical and Computational Applications,Vol. 15, No. 4, pp. 742-761, 21. c Association for Scientific Research CONSERVATION LAWS AND CONSERVED QUANTITIES FOR LAMINAR RADIAL JETS WITH SWIRL R. Naz 1,
More informationComputational Methods for Domains with! Complex Boundaries-I!
http://www.nd.edu/~gtrggva/cfd-course/ Computational Methods or Domains with Comple Boundaries-I Grétar Trggvason Spring For most engineering problems it is necessar to deal with comple geometries, consisting
More informationThe most common methods to identify velocity of flow are pathlines, streaklines and streamlines.
4 FLUID FLOW 4.1 Introduction Many civil engineering problems in fluid mechanics are concerned with fluids in motion. The distribution of potable water, the collection of domestic sewage and storm water,
More informationME 509, Spring 2016, Final Exam, Solutions
ME 509, Spring 2016, Final Exam, Solutions 05/03/2016 DON T BEGIN UNTIL YOU RE TOLD TO! Instructions: This exam is to be done independently in 120 minutes. You may use 2 pieces of letter-sized (8.5 11
More informationLecture 3 (Scalar and Vector Multiplication & 1D Motion) Physics Spring 2017 Douglas Fields
Lecture 3 (Scalar and Vector Multiplication & 1D Motion) Physics 160-02 Spring 2017 Douglas Fields Multiplication of Vectors OK, adding and subtracting vectors seemed fairly straightforward, but how would
More informationMathematical Modeling on MHD Free Convective Couette Flow between Two Vertical Porous Plates with Chemical Reaction and Soret Effect
International Journal of Advanced search in Phsical Science (IJARPS) Volume, Issue 5, September 4, PP 43-63 ISSN 349-7874 (Print) & ISSN 349-788 (Online) www.arcjournals.org Mathematical Modeling on MHD
More information18.325: Vortex Dynamics
8.35: Vortex Dynamics Problem Sheet. Fluid is barotropic which means p = p(. The Euler equation, in presence of a conservative body force, is Du Dt = p χ. This can be written, on use of a vector identity,
More informationChemical Reaction and Viscous Dissipation Effects on an Unsteady MHD Flow of Heat and Mass Transfer along a Porous Flat Plate
International Journal of Scientific and Innovative Mathematical Research (IJSIMR) Volume 2 Issue 2 December 24 PP 977-988 ISSN 2347-37X (Print) & ISSN 2347-342 (Online) www.arcjournals.org Chemical Reaction
More informationMMJ1153 COMPUTATIONAL METHOD IN SOLID MECHANICS PRELIMINARIES TO FEM
B Course Content: A INTRODUCTION AND OVERVIEW Numerical method and Computer-Aided Engineering; Phsical problems; Mathematical models; Finite element method;. B Elements and nodes, natural coordinates,
More informationENGI 9420 Engineering Analysis Solutions to Additional Exercises
ENGI 940 Engineering Analsis Solutions to Additional Exercises 0 Fall [Partial differential equations; Chapter 8] The function ux (, ) satisfies u u u + = 0, subject to the x x u x,0 = u x, =. Classif
More informationAvailable online at ScienceDirect. Procedia Engineering 90 (2014 )
Available online at.sciencedirect.com ScienceDirect Procedia Engineering 9 (14 383 388 1th International Conference on Mechanical Engineering, ICME 13 Effects of volumetric heat source and temperature
More informationV (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 informationScalar functions of several variables (Sect. 14.1)
Scalar functions of several variables (Sect. 14.1) Functions of several variables. On open, closed sets. Functions of two variables: Graph of the function. Level curves, contour curves. Functions of three
More informationMa 227 Final Exam Solutions 5/9/02
Ma 7 Final Exam Solutions 5/9/ Name: Lecture Section: I pledge m honor that I have abided b the Stevens Honor Sstem. ID: Directions: Answer all questions. The point value of each problem is indicated.
More informationFLUID MECHANICS. 1. Division of Fluid Mechanics. Hydrostatics Aerostatics Hydrodynamics Gasdynamics. v velocity p pressure ρ density
FLUID MECHANICS. Diision of Fluid Mechanics elocit p pressure densit Hdrostatics Aerostatics Hdrodnamics asdnamics. Properties of fluids Comparison of solid substances and fluids solid fluid τ F A [Pa]
More informationGUIDED WAVES IN A RECTANGULAR WAVE GUIDE
GUIDED WAVES IN A RECTANGULAR WAVE GUIDE Consider waves propagating along Oz but with restrictions in the and/or directions. The wave is now no longer necessaril transverse. The wave equation can be written
More informationIn this section, mathematical description of the motion of fluid elements moving in a flow field is
Jun. 05, 015 Chapter 6. Differential Analysis of Fluid Flow 6.1 Fluid Element Kinematics In this section, mathematical description of the motion of fluid elements moving in a flow field is given. A small
More informationLecture 5: 3-D Rotation Matrices.
3.7 Transformation Matri and Stiffness Matri in Three- Dimensional Space. The displacement vector d is a real vector entit. It is independent of the frame used to define it. d = d i + d j + d k = dˆ iˆ+
More informationFlight and Orbital Mechanics
Flight and Orbital Mechanics Lecture slides Challenge the future 1 Flight and Orbital Mechanics Lecture 7 Equations of motion Mark Voskuijl Semester 1-2012 Delft University of Technology Challenge the
More informationChapter 4. Motion in Two Dimensions
Chapter 4 Motion in Two Dimensions Kinematics in Two Dimensions Will study the vector nature of position, velocity and acceleration in greater detail Will treat projectile motion and uniform circular motion
More informationDo not turn over until you are told to do so by the Invigilator.
UNIVERSITY OF EAST ANGLIA School of Mathematics Main Series UG Examination 2014 15 FLUID DYNAMICS - THEORY AND COMPUTATION MTHA5002Y Time allowed: 3 Hours Attempt QUESTIONS 1 and 2, and THREE other questions.
More informationAA210A Fundamentals of Compressible Flow. Chapter 1 - Introduction to fluid flow
AA210A Fundamentals of Compressible Flow Chapter 1 - Introduction to fluid flow 1 1.2 Conservation of mass Mass flux in the x-direction [ ρu ] = M L 3 L T = M L 2 T Momentum per unit volume Mass per unit
More informationIntegration Past Papers Unit 2 Outcome 2
Integration Past Papers Unit 2 utcome 2 Multiple Choice Questions Each correct answer in this section is worth two marks.. Evaluate A. 2 B. 7 6 C. 2 D. 2 4 /2 d. 2. The diagram shows the area bounded b
More informationDefinition of Derivative
Definition of Derivative The derivative of the function f with respect to the variable x is the function ( ) fʹ x whose value at xis ( x) fʹ = lim provided the limit exists. h 0 ( + ) ( ) f x h f x h Slide
More informationHW6. 1. Book problems 8.5, 8.6, 8.9, 8.23, 8.31
HW6 1. Book problems 8.5, 8.6, 8.9, 8.3, 8.31. Add an equal strength sink and a source separated by a small distance, dx, and take the limit of dx approaching zero to obtain the following equations for
More informationMath 4381 / 6378 Symmetry Analysis
Math 438 / 6378 Smmetr Analsis Elementar ODE Review First Order Equations Ordinar differential equations of the form = F(x, ( are called first order ordinar differential equations. There are a variet of
More informationPhysics 101 Lecture 2 Vectors Dr. Ali ÖVGÜN
Phsics 101 Lecture 2 Vectors Dr. Ali ÖVGÜN EMU Phsics Department www.aovgun.com Coordinate Sstems qcartesian coordinate sstem qpolar coordinate sstem Januar 21, 2015 qfrom Cartesian to Polar coordinate
More information!! +! 2!! +!"!! =!! +! 2!! +!"!! +!!"!"!"
Homework 4 Solutions 1. (15 points) Bernoulli s equation can be adapted for use in evaluating unsteady flow conditions, such as those encountered during start- up processes. For example, consider the large
More informationQUESTION PAPER CODE 65/2/2/F EXPECTED ANSWER/VALUE POINTS
QUESTION PAPER CODE EXPECTED ANSWER/VALUE POINTS SECTION A. P 6 (A A ) P 6 9. (a b c) (a b c) 0 a b c (a b b c c a) 0 a b b c c a. a b sin θ a b cos θ 400 b 4 4. x z 5 or x z 5 mark for dc's of normal
More informationCHAPTER 3 Applications of Differentiation
CHAPTER Applications of Differentiation Section. Etrema on an Interval................... 0 Section. Rolle s Theorem and the Mean Value Theorem...... 0 Section. Increasing and Decreasing Functions and
More informationMATH MIDTERM 4 - SOME REVIEW PROBLEMS WITH SOLUTIONS Calculus, Fall 2017 Professor: Jared Speck. Problem 1. Approximate the integral
MATH 8. - MIDTERM 4 - SOME REVIEW PROBLEMS WITH SOLUTIONS 8. Calculus, Fall 7 Professor: Jared Speck Problem. Approimate the integral 4 d using first Simpson s rule with two equal intervals and then the
More informationContents. Dynamics and control of mechanical systems. Focuses on
Dnamics and control of mechanical sstems Date Da (/8) Da (3/8) Da 3 (5/8) Da 4 (7/8) Da 5 (9/8) Da 6 (/8) Content Review of the basics of mechanics. Kinematics of rigid bodies - coordinate transformation,
More informationDepartment of Aerospace Engineering AE602 Mathematics for Aerospace Engineers Assignment No. 6
Department of Aerospace Engineering AE Mathematics for Aerospace Engineers Assignment No.. Find the best least squares solution x to x, x 5. What error E is minimized? heck that the error vector ( x, 5
More informationMarking Scheme (Mathematics XII )
Sr. No. Marking Scheme (Mathematics XII 07-8) Answer Section A., (, ) A A: (, ) A A: (,),(,) Mark(s). -5. a iˆ, b ˆj. (or an other correct answer). 6 6 ( ), () ( ) ( ). Hence, is not associative. Section
More informationScalars distance speed mass time volume temperature work and energy
Scalars and Vectors scalar is a quantit which has no direction associated with it, such as mass, volume, time, and temperature. We sa that scalars have onl magnitude, or size. mass ma have a magnitude
More informationFIRST- AND SECOND-ORDER IVPS The problem given in (1) is also called an nth-order initial-value problem. For example, Solve: Solve:
.2 INITIAL-VALUE PROBLEMS 3.2 INITIAL-VALUE PROBLEMS REVIEW MATERIAL Normal form of a DE Solution of a DE Famil of solutions INTRODUCTION We are often interested in problems in which we seek a solution
More informationStreamline calculations. Lecture note 2
Streamline calculations. Lecture note 2 February 26, 2007 1 Recapitulation from previous lecture Definition of a streamline x(τ) = s(τ), dx(τ) dτ = v(x,t), x(0) = x 0 (1) Divergence free, irrotational
More informationLecture 17 Errors in Matlab s Turbulence PSD and Shaping Filter Expressions
Lectre 7 Errors in Matlab s Trblence PSD and Shaping Filter Expressions b Peter J Sherman /7/7 [prepared for AERE 355 class] In this brief note we will show that the trblence power spectral densities (psds)
More informationINTRODUCTION OBJECTIVES
INTRODUCTION The transport of particles in laminar and turbulent flows has numerous applications in engineering, biological and environmental systems. The deposition of aerosol particles in channels and
More informationOne-dimensional kinematics
Phsics 45 Formula Sheet Eam One-dimensional kinematics Vectors displacement: Δ f i total distance traveled average speed total time Δ f i average velocit: vav t f ti Δ instantaneous velocit: v lim Δ t
More informationChemical Reaction, Radiation and Dufour Effects on Casson Magneto Hydro Dynamics Fluid Flow over A Vertical Plate with Heat Source/Sink
Global Journal of Pure and Applied Mathematics. ISSN 973-768 Volume, Number (6), pp. 9- Research India Publications http://www.ripublication.com Chemical Reaction, Radiation and Dufour Effects on Casson
More informationTHE HEATED LAMINAR VERTICAL JET IN A LIQUID WITH POWER-LAW TEMPERATURE DEPENDENCE OF DENSITY. V. A. Sharifulin.
THE HEATED LAMINAR VERTICAL JET IN A LIQUID WITH POWER-LAW TEMPERATURE DEPENDENCE OF DENSITY 1. Introduction V. A. Sharifulin Perm State Technical Universit, Perm, Russia e-mail: sharifulin@perm.ru Water
More informationVectors. Introduction
Chapter 3 Vectors Vectors Vector quantities Physical quantities that have both numerical and directional properties Mathematical operations of vectors in this chapter Addition Subtraction Introduction
More informationMath Review Night: Work and the Dot Product
Math Review Night: Work and the Dot Product Dot Product A scalar quantity Magnitude: A B = A B cosθ The dot product can be positive, zero, or negative Two types of projections: the dot product is the parallel
More informationIntroduction to Differential Equations. National Chiao Tung University Chun-Jen Tsai 9/14/2011
Introduction to Differential Equations National Chiao Tung Universit Chun-Jen Tsai 9/14/011 Differential Equations Definition: An equation containing the derivatives of one or more dependent variables,
More informationPhysics of Tsunamis. This is an article from my home page: Ole Witt-Hansen 2011 (2016)
Phsics of Tsunamis This is an article from m home page: www.olewitthansen.dk Ole Witt-Hansen 11 (16) Contents 1. Constructing a differential equation for the Tsunami wave...1. The velocit of propagation
More informationME 321: FLUID MECHANICS-I
6/07/08 ME 3: LUID MECHANI-I Dr. A.B.M. Toufique Hasan Professor Department of Mechanical Engineering Bangladesh Universit of Engineering & Technolog (BUET), Dhaka Lecture- 4/07/08 Momentum Principle teacher.buet.ac.bd/toufiquehasan/
More informationHigh resolution of 2D natural convection in a cavity by the DQ method
Journal of Computational and Applied Mathematics 7) 9 6 www.elsevier.com/locate/cam High resolution of D natural convection in a cavit b the DQ method D.C. Lo a,, D.L. Young b, C.C. Tsai c a Department
More informationJoule Heating Effects on MHD Natural Convection Flows in Presence of Pressure Stress Work and Viscous Dissipation from a Horizontal Circular Cylinder
Journal of Applied Fluid Mechanics, Vol. 7, No., pp. 7-3, 04. Available online at www.jafmonline.net, ISSN 735-357, EISSN 735-3645. Joule Heating Effects on MHD Natural Convection Flows in Presence of
More informationCONSERVATION OF ANGULAR MOMENTUM FOR A CONTINUUM
Chapter 4 CONSERVATION OF ANGULAR MOMENTUM FOR A CONTINUUM Figure 4.1: 4.1 Conservation of Angular Momentum Angular momentum is defined as the moment of the linear momentum about some spatial reference
More informationChapter 2: Pressure Distribution in a Fluid
58:6 Chapter Professor Fred Stern Fall 6 Chapter : Pressure Distribution in a Fluid Pressure and pressure gradient In fluid statics, as well as in fluid dnamics, the forces acting on a portion of fluid
More informationSPS Mathematical Methods
SPS 2281 - Mathematical Methods Assignment No. 2 Deadline: 11th March 2015, before 4:45 p.m. INSTRUCTIONS: Answer the following questions. Check our answer for odd number questions at the back of the tetbook.
More informationFluid Dynamics Exercises and questions for the course
Fluid Dynamics Exercises and questions for the course January 15, 2014 A two dimensional flow field characterised by the following velocity components in polar coordinates is called a free vortex: u r
More informationChapter 4. Motion in Two Dimensions. Position and Displacement. General Motion Ideas. Motion in Two Dimensions
Motion in Two Dimensions Chapter 4 Motion in Two Dimensions Using + or signs is not always sufficient to fully describe motion in more than one dimension Vectors can be used to more fully describe motion
More informationIntroduction to vectors
Lecture 4 Introduction to vectors Course website: http://facult.uml.edu/andri_danlov/teaching/phsicsi Lecture Capture: http://echo360.uml.edu/danlov2013/phsics1fall.html 95.141, Fall 2013, Lecture 3 Outline
More informationOrdinary Differential Equations n
Numerical Analsis MTH63 Ordinar Differential Equations Introduction Talor Series Euler Method Runge-Kutta Method Predictor Corrector Method Introduction Man problems in science and engineering when formulated
More informationProgressive wave: a new multisource vibration technique to assist forming processes - kinematic study, simulation results and design proposition
Progressive wave: a new multisource vibration technique to assist forming processes - kinematic stud, simulation results and design proposition A. Khan a, T. H. Nguen a, C. Giraud-Audine a, G. Abba b,
More information5.6. Differential equations
5.6. Differential equations The relationship between cause and effect in phsical phenomena can often be formulated using differential equations which describe how a phsical measure () and its derivative
More informationParticular Solutions
Particular Solutions Our eamples so far in this section have involved some constant of integration, K. We now move on to see particular solutions, where we know some boundar conditions and we substitute
More informationChapter 2: Pressure Distribution in a Fluid
ME:56 Chapter Professor Fred Stern Fall 7 Chapter : Pressure Distribution in a Fluid Pressure and pressure gradient In fluid statics, as well as in fluid dnamics, the forces acting on a portion of fluid
More informationThe Control-Volume Finite-Difference Approximation to the Diffusion Equation
The Control-Volume Finite-Difference Approimation to the Diffusion Equation ME 448/548 Notes Gerald Recktenwald Portland State Universit Department of Mechanical Engineering gerr@mepdedu ME 448/548: D
More information