Chapter 3 Cartesian Vectors and Tensors: Their Calculus
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General Meteorology
Dynamic Meteorology 2 Lecture 9 Sahraei Physics Department Razi University http://www.razi.ac.ir/sahraei Stream Function Incompressible fluid uv 0 xy u ; v Definition of Stream Function y x Substituting these in the irrotationality condition, we have vu 0 xy 22 0 xy22 Velocity Potential Irrotational flow vu Since the, V 0 V 0 0 the flow field is irrotational. xy u ; v Definition of Velocity Potential x y Velocity potential is a powerful tool in analysing irrotational flows. Continuity Equation 22 uv 2 0 0 0 xy xy22 As with stream functions we can have lines along which potential is constant. These are called Equipotential Lines of the flow. Thus along a potential line c Flow along a line l Consider a fluid particle moving along a line l . dx For each small displacement dl dy dl idxˆˆ jdy Where iˆ and ˆj are unit vectors in the x and y directions, respectively. Since dl is parallel to V , then the cross product must be zero. V iuˆˆ jv V dl iuˆ ˆjv idx ˆ ˆjdy udy vdx kˆ 0 dx dy uv Stream Function dx dy l Since must be satisfied along a line , such a line is called a uv dl streamline or flow line. A mathematical construct called a stream function can describe flow associated with these lines. The Stream Function xy, is defined as the function which is constant along a streamline, much as a potential function is constant along an equipotential line. Since xy, is constant along a flow line, then for any , d dx dy 0 along the streamline xy Stream Functions d dx dy 0 dx dy xy xy dx dy vdx ud y uv uv , from which we can see that yx So that if one can find the stream function, one can get the discharge by differentiation. -
Potential Flow Theory
2.016 Hydrodynamics Reading #4 2.016 Hydrodynamics Prof. A.H. Techet Potential Flow Theory “When a flow is both frictionless and irrotational, pleasant things happen.” –F.M. White, Fluid Mechanics 4th ed. We can treat external flows around bodies as invicid (i.e. frictionless) and irrotational (i.e. the fluid particles are not rotating). This is because the viscous effects are limited to a thin layer next to the body called the boundary layer. In graduate classes like 2.25, you’ll learn how to solve for the invicid flow and then correct this within the boundary layer by considering viscosity. For now, let’s just learn how to solve for the invicid flow. We can define a potential function,!(x, z,t) , as a continuous function that satisfies the basic laws of fluid mechanics: conservation of mass and momentum, assuming incompressible, inviscid and irrotational flow. There is a vector identity (prove it for yourself!) that states for any scalar, ", " # "$ = 0 By definition, for irrotational flow, r ! " #V = 0 Therefore ! r V = "# ! where ! = !(x, y, z,t) is the velocity potential function. Such that the components of velocity in Cartesian coordinates, as functions of space and time, are ! "! "! "! u = , v = and w = (4.1) dx dy dz version 1.0 updated 9/22/2005 -1- ©2005 A. Techet 2.016 Hydrodynamics Reading #4 Laplace Equation The velocity must still satisfy the conservation of mass equation. We can substitute in the relationship between potential and velocity and arrive at the Laplace Equation, which we will revisit in our discussion on linear waves. -
A Brief Tour of Vector Calculus
A BRIEF TOUR OF VECTOR CALCULUS A. HAVENS Contents 0 Prelude ii 1 Directional Derivatives, the Gradient and the Del Operator 1 1.1 Conceptual Review: Directional Derivatives and the Gradient........... 1 1.2 The Gradient as a Vector Field............................ 5 1.3 The Gradient Flow and Critical Points ....................... 10 1.4 The Del Operator and the Gradient in Other Coordinates*............ 17 1.5 Problems........................................ 21 2 Vector Fields in Low Dimensions 26 2 3 2.1 General Vector Fields in Domains of R and R . 26 2.2 Flows and Integral Curves .............................. 31 2.3 Conservative Vector Fields and Potentials...................... 32 2.4 Vector Fields from Frames*.............................. 37 2.5 Divergence, Curl, Jacobians, and the Laplacian................... 41 2.6 Parametrized Surfaces and Coordinate Vector Fields*............... 48 2.7 Tangent Vectors, Normal Vectors, and Orientations*................ 52 2.8 Problems........................................ 58 3 Line Integrals 66 3.1 Defining Scalar Line Integrals............................. 66 3.2 Line Integrals in Vector Fields ............................ 75 3.3 Work in a Force Field................................. 78 3.4 The Fundamental Theorem of Line Integrals .................... 79 3.5 Motion in Conservative Force Fields Conserves Energy .............. 81 3.6 Path Independence and Corollaries of the Fundamental Theorem......... 82 3.7 Green's Theorem.................................... 84 3.8 Problems........................................ 89 4 Surface Integrals, Flux, and Fundamental Theorems 93 4.1 Surface Integrals of Scalar Fields........................... 93 4.2 Flux........................................... 96 4.3 The Gradient, Divergence, and Curl Operators Via Limits* . 103 4.4 The Stokes-Kelvin Theorem..............................108 4.5 The Divergence Theorem ...............................112 4.6 Problems........................................114 List of Figures 117 i 11/14/19 Multivariate Calculus: Vector Calculus Havens 0. -
Stream Function for Incompressible 2D Fluid
26/3/2020 Navier–Stokes equations - Wikipedia Continuity equation for incompressible fluid Regardless of the flow assumptions, a statement of the conservation of mass is generally necessary. This is achieved through the mass continuity equation, given in its most general form as: or, using the substantive derivative: For incompressible fluid, density along the line of flow remains constant over time, therefore divergence of velocity is null all the time Stream function for incompressible 2D fluid Taking the curl of the incompressible Navier–Stokes equation results in the elimination of pressure. This is especially easy to see if 2D Cartesian flow is assumed (like in the degenerate 3D case with uz = 0 and no dependence of anything on z), where the equations reduce to: Differentiating the first with respect to y, the second with respect to x and subtracting the resulting equations will eliminate pressure and any conservative force. For incompressible flow, defining the stream function ψ through results in mass continuity being unconditionally satisfied (given the stream function is continuous), and then incompressible Newtonian 2D momentum and mass conservation condense into one equation: 4 μ where ∇ is the 2D biharmonic operator and ν is the kinematic viscosity, ν = ρ. We can also express this compactly using the Jacobian determinant: https://en.wikipedia.org/wiki/Navier–Stokes_equations 1/2 26/3/2020 Navier–Stokes equations - Wikipedia This single equation together with appropriate boundary conditions describes 2D fluid flow, taking only kinematic viscosity as a parameter. Note that the equation for creeping flow results when the left side is assumed zero. In axisymmetric flow another stream function formulation, called the Stokes stream function, can be used to describe the velocity components of an incompressible flow with one scalar function. -
A Dual-Potential Formulation of the Navier-Stokes Equations Steven Gerard Gegg Iowa State University
Iowa State University Capstones, Theses and Retrospective Theses and Dissertations Dissertations 1989 A dual-potential formulation of the Navier-Stokes equations Steven Gerard Gegg Iowa State University Follow this and additional works at: https://lib.dr.iastate.edu/rtd Part of the Aerospace Engineering Commons, and the Mechanical Engineering Commons Recommended Citation Gegg, Steven Gerard, "A dual-potential formulation of the Navier-Stokes equations " (1989). Retrospective Theses and Dissertations. 9040. https://lib.dr.iastate.edu/rtd/9040 This Dissertation is brought to you for free and open access by the Iowa State University Capstones, Theses and Dissertations at Iowa State University Digital Repository. It has been accepted for inclusion in Retrospective Theses and Dissertations by an authorized administrator of Iowa State University Digital Repository. For more information, please contact [email protected]. INFORMATION TO USERS The most advanced technology has been used to photo graph and reproduce this manuscript from the microfilm master. UMI films the text directly from the original or copy submitted. Thus, some thesis and dissertation copies are in typewriter face, while others may be from any type of computer printer. The quality of this reproduction is dependent upon the quality of the copy submitted. Broken or indistinct print, colored or poor quality illustrations and photographs, print bleedthrough, substandard margins, and improper alignment can adversely affect reproduction. In the unlikely event that the author did not send UMI a complete manuscript and there are missing pages, these will be noted. Also, if unauthorized copyright material had to be removed, a note will indicate the deletion. Oversize materials (e.g., maps, drawings, charts) are re produced by sectioning the original, beginning at the upper left-hand corner and continuing from left to right in equal sections with small overlaps. -
Div-Curl Problems and H1-Regular Stream Functions in 3D Lipschitz Domains
Received 21 May 2020; Revised 01 February 2021; Accepted: 00 Month 0000 DOI: xxx/xxxx PREPRINT Div-Curl Problems and H1-regular Stream Functions in 3D Lipschitz Domains Matthias Kirchhart1 | Erick Schulz2 1Applied and Computational Mathematics, RWTH Aachen, Germany Abstract 2Seminar in Applied Mathematics, We consider the problem of recovering the divergence-free velocity field U Ë L2(Ω) ETH Zürich, Switzerland of a given vorticity F = curl U on a bounded Lipschitz domain Ω Ï R3. To that end, Correspondence we solve the “div-curl problem” for a given F Ë H*1(Ω). The solution is expressed in Matthias Kirchhart, Email: 1 [email protected] terms of a vector potential (or stream function) A Ë H (Ω) such that U = curl A. After discussing existence and uniqueness of solutions and associated vector potentials, Present Address Applied and Computational Mathematics we propose a well-posed construction for the stream function. A numerical method RWTH Aachen based on this construction is presented, and experiments confirm that the resulting Schinkelstraße 2 52062 Aachen approximations display higher regularity than those of another common approach. Germany KEYWORDS: div-curl system, stream function, vector potential, regularity, vorticity 1 INTRODUCTION Let Ω Ï R3 be a bounded Lipschitz domain. Given a vorticity field F .x/ Ë R3 defined over Ω, we are interested in solving the problem of velocity recovery: T curl U = F in Ω. (1) div U = 0 This problem naturally arises in fluid mechanics when studying the vorticity formulation of the incompressible Navier–Stokes equations. Vortex methods, for example, are based on the vorticity formulation and require a solution of problem (1) at every time-step. -
Useful Identities and Theorems from Vector Calculus
Appendix A Useful Identities and Theorems from Vector Calculus A.1 Vector Identities A · (B × C) = C · (A × B) = B · (C × A) A × (B × C) = B(A · C) − C(A · B) (A × B) × C = B(A · C) − A(B · C) ∇×∇f = 0 ∇·(∇×A) = 0 ∇·( f A) = (∇ f ) · A + f (∇·A) ∇×( f A) = (∇ f ) × A + f (∇×A) ∇·(A × B) = B · (∇×A) − A · (∇×B) ∇(A · B) = (B ·∇)A + (A ·∇)B + B × (∇×A) + A × (∇×B) ∇·(AB) = (A ·∇)B + B(∇·A) ∇×(A × B) = (B ·∇)A − (A ·∇)B − B(∇·A) + A(∇·B) ∇×(∇×A) =∇(∇·A) −∇2 A A.2 The Gradient Theorem For two points a, b in a space where a scalar function f with spatial derivatives everywhere well-defined up to first order, b (∇ f ) · d = f (b) − f (a), a independently of the integration path between a and b. P. Charbonneau, Solar and Stellar Dynamos, Saas-Fee Advanced Course 39, 215 DOI: 10.1007/978-3-642-32093-4, © Springer-Verlag Berlin Heidelberg 2013 216 Appendix A: Useful Identities and Theorems from Vector Calculus A.3 The Divergence Theorem For any vector field A with spatial derivatives of all its scalar components everywhere well-defined up to first order, (∇·A)dV = A · nˆ dS , V S where the surface S encloses the volume V . A.4 Stokes’ Theorem For any vector field A with spatial derivatives of all its scalar components everywhere well-defined up to first order, (∇×A) · nˆ dS = A · d , S γ where the contour γ delimits the surface S, and the orientation of the unit nor- mal vector nˆ and direction of contour integration are mutually linked by the right-hand rule. -
Part IA — Vector Calculus
Part IA | Vector Calculus Based on lectures by B. Allanach Notes taken by Dexter Chua Lent 2015 These notes are not endorsed by the lecturers, and I have modified them (often significantly) after lectures. They are nowhere near accurate representations of what was actually lectured, and in particular, all errors are almost surely mine. 3 Curves in R 3 Parameterised curves and arc length, tangents and normals to curves in R , the radius of curvature. [1] 2 3 Integration in R and R Line integrals. Surface and volume integrals: definitions, examples using Cartesian, cylindrical and spherical coordinates; change of variables. [4] Vector operators Directional derivatives. The gradient of a real-valued function: definition; interpretation as normal to level surfaces; examples including the use of cylindrical, spherical *and general orthogonal curvilinear* coordinates. Divergence, curl and r2 in Cartesian coordinates, examples; formulae for these oper- ators (statement only) in cylindrical, spherical *and general orthogonal curvilinear* coordinates. Solenoidal fields, irrotational fields and conservative fields; scalar potentials. Vector derivative identities. [5] Integration theorems Divergence theorem, Green's theorem, Stokes's theorem, Green's second theorem: statements; informal proofs; examples; application to fluid dynamics, and to electro- magnetism including statement of Maxwell's equations. [5] Laplace's equation 2 3 Laplace's equation in R and R : uniqueness theorem and maximum principle. Solution of Poisson's equation by Gauss's method (for spherical and cylindrical symmetry) and as an integral. [4] 3 Cartesian tensors in R Tensor transformation laws, addition, multiplication, contraction, with emphasis on tensors of second rank. Isotropic second and third rank tensors. -
Generalized Stokes' Theorem
Chapter 4 Generalized Stokes’ Theorem “It is very difficult for us, placed as we have been from earliest childhood in a condition of training, to say what would have been our feelings had such training never taken place.” Sir George Stokes, 1st Baronet 4.1. Manifolds with Boundary We have seen in the Chapter 3 that Green’s, Stokes’ and Divergence Theorem in Multivariable Calculus can be unified together using the language of differential forms. In this chapter, we will generalize Stokes’ Theorem to higher dimensional and abstract manifolds. These classic theorems and their generalizations concern about an integral over a manifold with an integral over its boundary. In this section, we will first rigorously define the notion of a boundary for abstract manifolds. Heuristically, an interior point of a manifold locally looks like a ball in Euclidean space, whereas a boundary point locally looks like an upper-half space. n 4.1.1. Smooth Functions on Upper-Half Spaces. From now on, we denote R+ := n n f(u1, ... , un) 2 R : un ≥ 0g which is the upper-half space of R . Under the subspace n n n topology, we say a subset V ⊂ R+ is open in R+ if there exists a set Ve ⊂ R open in n n n R such that V = Ve \ R+. It is intuitively clear that if V ⊂ R+ is disjoint from the n n n subspace fun = 0g of R , then V is open in R+ if and only if V is open in R . n n Now consider a set V ⊂ R+ which is open in R+ and that V \ fun = 0g 6= Æ. -
LECTURE 27: the LAPLAST ONE Monday, November 25, 2019 5:23 PM
LECTURE 27: THE LAPLAST ONE Monday, November 25, 2019 5:23 PM Today: Three little remaining topics related to Laplace I- 3 DIMENSIONS Previously: Solved Laplace's equation in 2 dimensions by converting it into polar coordinates. The same idea works in 3 dimensions if you use spherical coordinates. 3 Suppose u = u(x,y,z) solves u xx + u yy + u zz = 0 in R Using spherical coordinates, you eventually get urr + 2 ur + JUNK = 0 r (where r = x 2 + y 2 + z 2 and JUNK doesn't depend on r) If we're looking for radial solutions, we set JUNK = 0 Get u rr + 2 u r = 0 which you can solve to get r u(x,y,z) = -C + C' solves u xx + u yy + u zz = 0 r Finally, setting C = -1/(4π) and C' = 0, you get Fundamental solution of Laplace for n = 3 S(x,y,z) = 1 = 4πr 4π x 2 + y 2 + z 2 Note: In n dimensions, get u rr + n-1 ur = 0 r => u( r ) = -C + C' rn-2 => S(x) = Blah (for some complicated Blah) rn-1 Why fundamental? Because can build up other solutions from this! Fun Fact: A solution of -Δ u = f (Poisson's equation) in R n is u(x) = S(x) * f(x) = S(x -y) f(y) dy (Basically the constant is chosen such that -ΔS = d0 <- Dirac at 0) II - DERIVATION OF LAPLACE Two goals: Derive Laplace's equation, and also highlight an important structure of Δu = 0 A) SETTING n Definition: If F = (F 1, …, F n) is a vector field in R , then div(F) = (F 1)x1 + … + (F n)xn Notice : If u = u(x 1, …, x n), then u = (u x1 , …, u xn ) => div( u) = (u x1 )x1 + … + (u xn )xn = u x1 x1 + … + u xn xn = Δu Fact: Δu = div( u) "divergence structure" In particular, Laplace's equation works very well with the divergence theorem Divergence Theorem: F n dS = div(F) dx bdy D D B) DERIVATION Suppose you have a fluid F that is in equilibrium (think F = temperature or chemical concentration) Equilibrium means that for any region D, the net flux of F is 0. -
Green Gauss Theorem Yesterday, We Continued Discussions on Index Notations That Can Be Used to Represent Tensors
15/02/2017 LECTURE – 15 Green Gauss Theorem Yesterday, we continued discussions on index notations that can be used to represent tensors. In index notations we saw the Gradient of a scalar Divergence of a vector Cross product of vector etc. We also saw that a second rank tensor can be written as a sum of a symmetric & asymmetric tensor. 11 i.e, BBBBB[][] ij22 ij ji ij ji First part is symmetric & second part is asymmetric Today we will briefly discuss about Green Gauss Theorem etc. Green Gauss Theorem relates the volume & surface integrals. The most common form of Gauss’s theorem is the Gauss divergence theorem which you have studied in previous courses. 푛 푣 ds If you have a volume U formed by surface S, the Gauss divergence theorem for a vector v suggest that v.. ndSˆ vdU SU where, S = bounding surface on closed surface U = volumetric domain nˆ = the unit outward normal vector of the elementary surface area ds This Gauss Divergence theorem can also be represented using index notations. v v n dS i dU ii SUxi For any scalar multiple or factor for vector v , say v , the Green Gauss can be represented as (v . nˆ ) dS .( v ) dU SU i.e. (v . nˆ ) dS ( . v ) dU ( v . ) dU SUU v or v n dSi dU v dU i i i SUUxxii Gauss’s theorem is applicable not only to a vector . It can be applied to any tensor B (say) B B n dSij dU B dU ij i ij SUUxxii Stoke’s Theorem Stoke’s theorem relates the integral over an open surface S, to line integral around the surface’s bounding curve (say C) You need to appropriately choose the unit outward normal vector to the surface 푛 푡 dr v. -
Vector Calculus Applicationsž 1. Introduction 2. the Heat Equation
Vector Calculus Applications 1. Introduction The divergence and Stokes’ theorems (and their related results) supply fundamental tools which can be used to derive equations which can be used to model a number of physical situations. Essentially, these theorems provide a mathematical language with which to express physical laws such as conservation of mass, momentum and energy. The resulting equations are some of the most fundamental and useful in engineering and applied science. In the following sections the derivation of some of these equations will be outlined. The goal is to show how vector calculus is used in applications. Generally speaking, the equations are derived by first using a conservation law in integral form, and then converting the integral form to a differential equation form using the divergence theorem, Stokes’ theorem, and vector identities. The differential equation forms tend to be easier to work with, particularly if one is interested in solving such equations, either analytically or numerically. 2. The Heat Equation Consider a solid material occupying a region of space V . The region has a boundary surface, which we shall designate as S. Suppose the solid has a density and a heat capacity c. If the temperature of the solid at any point in V is T.r; t/, where r x{ y| zkO is the position vector (so that T depends upon x, y, z and t), then theE total heatE eergyD O containedC O C in the solid is • cT dV : V Heat energy can get in or out of the region V by flowing across the boundary S, or it can be generated inside V .