Overview

Part 21 - Summary

Limits

Let’s compare limits in one variable to several.

lim⁡x→af(x)=L\lim_{x \to a} f(x) = L lim⁡(x,y)→(a,b)f(x,y)=L\lim_{(x, y) \to (a, b)} f(x, y) = L

They work quite similar, let’s see the limit laws:

lim⁡(x,y)→(a,b)f(x,y)±h(x,y)=L±M\lim_{(x, y) \to (a, b)} f(x, y) \pm h(x, y) = L \pm M
lim⁡(x,y)→(a,b)f(x,y)⋅h(x,y)=L⋅M\lim_{(x, y) \to (a, b)} f(x, y) \cdot h(x, y) = L \cdot M
lim⁡(x,y)→(a,b)f(x,y)h(x,y)=LM,M≠0\lim_{(x, y) \to (a, b)} \dfrac{f(x, y)}{h(x, y)} = \dfrac{L}{M}, \quad M \neq 0

Partial derivative

Recall (Partial derivative)

The partial derivative of a function of two variables with respect to xx, denoted by fxf_x, is the function of two variables given by:

fx(x,y)=lim⁡h→0f(x+h,y)−f(x,y)hf_x(x, y) = \lim_{h \to 0} \dfrac{f(x + h, y) - f(x, y)}{h}

Similarly for yy:

fy(x,y)=lim⁡h→0f(x,y+h)−f(x,y)hf_y(x, y) = \lim_{h \to 0} \dfrac{f(x, y + h) - f(x, y)}{h}

Chain rule

Recall (Chain rule)

Suppose z=f(x,y)z = f(x, y) is differentiable function of x,yx, y. Where x=g(t)x = g(t) and y=h(t)y = h(t). Which both are differentiable functions of tt. Then:

dzdt=∂z∂xdxdt+∂z∂ydydt\boxed{\dfrac{dz}{dt} = \dfrac{\partial z}{\partial x} \dfrac{dx}{dt} + \dfrac{\partial z}{\partial y} \dfrac{dy}{dt}}

General chain rule

Recall (General chain rule)

Let zz be a differentiable function of nn variables, x1,…,xnx_1, \ldots, x_n, where each xix_i is differentiable function of mm variables, t1,…,tmt_1, \ldots, t_m.

Then:

∂z∂ti=∂z∂x1∂x1∂ti+∂z∂x2∂x2∂ti+…+∂z∂xn∂xn∂ti\dfrac{\partial z}{\partial t_i} = \dfrac{\partial z}{\partial x_1} \dfrac{\partial x_1}{\partial t_i} + \dfrac{\partial z}{\partial x_2} \dfrac{\partial x_2}{\partial t_i} + \ldots + \dfrac{\partial z}{\partial x_n} \dfrac{\partial x_n}{\partial t_i}

Implicit differentiation

Recall (Implicit differentiation)

Suppose a function y=y(x)y = y(x) is given implicitly by equation of the form F(x,y)=0F(x, y) = 0 where FF is a differentiable function of two variables and Fy≠0F_y \neq 0. Then:

dydx=−FxFy\boxed{\dfrac{dy}{dx} = -\dfrac{F_x}{F_y}}

Implicit differentiation of several variables

Recall (Implicit differentiation of several variables)

Let z(x,y)z(x, y) be given implicitly, by equation of form F(x,y,z)=0F(x, y, z) = 0 where FF is differentiable and Fz≠0F_z \neq 0, then:

∂z∂x=−FxFz,∂z∂y=−FyFz.\begin{align*} \dfrac{\partial z}{\partial x} & = -\dfrac{F_x}{F_z}, \newline \dfrac{\partial z}{\partial y} & = -\dfrac{F_y}{F_z}. \end{align*}

Definition of directional derivatives

The directional derivative of a function, ff, of two variables, at point (x0,y0)(x_0, y_0) in the direction of a unit vector, u⃗\vec{u}.

u⃗=⟨a,b⟩\vec{u} = \langle a, b \rangle

We denoted the directional derivative with a Du⃗fD_{\vec{u}} f.

Du⃗f(x0,y0)=lim⁡h→0f(x0+ha,y0+hb)−f(x0,y0)hD_{\vec{u}} f(x_0, y_0) = \lim_{h \to 0} \dfrac{f(x_0 + ha, y_0 + hb) - f(x_0, y_0)}{h}

Definition of gradient

The gradient of, ff, is the vector-function:

∇f=⟨fx,fy⟩\nabla f = \langle f_x, f_y \rangle

Therefore, we usually write:

Du⃗f=∇f⋅u⃗\boxed{D_{\vec{u}} f = \nabla f \cdot \vec{u}}

Maximum rate of change

If we ask ourselves the question, in what direction is Du⃗f(x0,y0)D_{\vec{u}} f(x_0, y_0) the largest?

If we look at the definition:

Du⃗f(x0,y0)=∇f(x0,y0)⋅u⃗D_{\vec{u}} f(x_0, y_0) = \nabla f(x_0, y_0) \cdot \vec{u}

If we use the geometrical definition:

Du⃗f(x0,y0)=∣∇f(x0,y0)∣∣u⃗∣cos⁡(α)D_{\vec{u}} f(x_0, y_0) = |\nabla f(x_0, y_0)| |\vec{u}| \cos(\alpha)

Gradient and level curves

Recall that level curves are curves with the equation:

f(x,y)=kf(x, y) = k

Where kk is just any constant. For each point (x0,y0)(x_0, y_0), ∇f(x0,y0)\nabla f(x_0, y_0) is orthogonal to the level curve that contains (x0,y0)(x_0, y_0)

Critical points

(a,b)(a, b) is a critical point if ∇f(a,b)=0 or ∇f(a,b)∄\nabla f(a, b) = 0 \textbf{ or } \nabla f(a, b) \nexists

In other words, if (a,b)(a, b) is a critical point of local minimum/maximum then it is a critical point.

However, the other way around this implication is not true. A critical point might not be a local minimum/maximum.

2nd derivative test for functions of two variables

Suppose (a,b)(a, b) is a critical point of a function, ff, of two variables. Suppose 2nd order partial derivatives exists and are continuous.

Let D=D(a,b)=fxx(a,b)fyy(a,b)−(fxy(a,b))2D = D(a, b) = f_{xx}(a, b) f_{yy}(a,b) - \left(f_{xy} (a,b)\right)^2

Then:

D>0 and fxx(a,b)>0local minimum,D>0 and fxx(a,b)<0local maximum,D<0neither, this is a saddle point.\begin{align*} D > 0 \text{ and } f_{xx}(a, b) > 0 & \quad \text{local minimum}, \newline D > 0 \text{ and } f_{xx}(a, b) < 0 & \quad \text{local maximum}, \newline D < 0 & \quad \text{neither, this is a saddle point}. \end{align*}

Lagrange multiplier method

Recall (Lagrange multiplier method)

To find minimum/maximum values of function, ff, subject to constraint, g(x,y)=kg(x, y) = k, assuming minimum/maximum points exists and ∇g≠0\nabla g \neq 0

  1. Find all numbers x,yx, y and λ\lambda, such that:

    ∇f(x,y)=λ∇g(x,y),g(x,y)=k.\nabla f(x, y) = \lambda \nabla g(x, y), \quad g(x, y) = k.
  2. Compute values from step 1, choose the minimum/maximum value(s).

Type I region definition

If DD is of type I, then:

∬Df(x,y) dA=∫ab∫g1(x)g2(x)f(x,y) dy dx\iint_D f(x, y) \, dA = \int_a^b \int_{g_1(x)}^{g_2(x)} f(x, y) \, dy \, dx

Type II region definition

If DD is of type II, then:

∬Df(x,y) dA=∫cd∫h1(y)h2(y)f(x,y) dx dy\iint_D f(x, y) \, dA = \int_c^d \int_{h_1(y)}^{h_2(y)} f(x, y) \, dx \, dy

General case of variable change

∬Df(x,y) dA\iint_D f(x, y) \, dA

We want to rewrite this in terms of uu and vv. Let’s say that:

x=g(u,v),y=h(u,v).x = g(u, v), \quad y = h(u, v).

We can say that we have a transformation, TT, from the uvuv-plane to the xyxy-plane, given by our functions gg and hh.

We need to make some assumptions of TT to make our lives easier.

  1. TT is a C1C^1-transformation, meaning that gg and hh have continuous partial derivatives.

  2. TT is an injective transformation (meaning it is 1-to-1). This means that we can express uu and vv in terms of xx and yy.

The Jacobian matrix of a transformation, TT, is:

∂(x,y)∂(u,v)=det⁡[∂x∂u∂x∂v∂y∂u∂y∂v]\dfrac{\partial(x, y)}{\partial(u, v)} = \det \begin{bmatrix} \dfrac{\partial x}{\partial u} & \dfrac{\partial x}{\partial v} \newline \dfrac{\partial y}{\partial u} & \dfrac{\partial y}{\partial v} \end{bmatrix}

Suppose TT is a transformation, from the uvuv-plane to the xyxy-plane. Assuming that the Jacobian for TT, is non-zero, then:

∬Df(x,y) dA=∬Sf(x(u,v),y(u,v))∣∂(x,y)∂(u,v)∣ dA.\iint_D f(x, y) \, dA = \iint_S f(x(u, v), y(u, v)) \left\vert \tfrac{\partial(x, y)}{\partial(u, v)} \right\vert \, dA.

In three variables

Let x=x(u,v,w),y=y(u,v,w),z=z(u,v,w)x = x(u, v, w), y = y(u, v, w), z = z(u, v, w)

The Jacobian is:

∂(x,y,z)∂(u,v,w)=det⁡[∂x∂u∂x∂v∂x∂w∂y∂u∂y∂v∂y∂w∂z∂u∂z∂v∂z∂w]\dfrac{\partial(x, y, z)}{\partial(u, v, w)} = \det \begin{bmatrix} \dfrac{\partial x}{\partial u} & \dfrac{\partial x}{\partial v} & \dfrac{\partial x}{\partial w} \newline \dfrac{\partial y}{\partial u} & \dfrac{\partial y}{\partial v} & \dfrac{\partial y}{\partial w} \newline \dfrac{\partial z}{\partial u} & \dfrac{\partial z}{\partial v} & \dfrac{\partial z}{\partial w} \end{bmatrix}

Just as we did before:

∭Ef(x,y,z) dV=∭Sf(x(u,v,w),y(u,v,w),z(u,v,w))∣∂(x,y,z)∂(u,v,w)∣ dV.\iiint_E f(x, y, z) \, dV = \iiint_S f(x(u, v, w), y(u, v, w), z(u, v, w)) \left\vert \tfrac{\partial(x, y, z)}{\partial(u, v, w)} \right\vert \, dV.

Polar coordinates

∬Sg(r,θ) dA=∬Sf(rcos⁡(θ),rsin⁡(θ))⋅r dA\iint_S g(r, \theta) \, dA = \iint_S f(r \cos(\theta), r \sin(\theta)) \cdot r \, dA

It makes sense to change to polar coordinates if we have a circle/circle like shape.

Cylindrical coordinates

∭Ef(x,y,z) dV=∭Sf(rcos⁡(θ),rsin⁡(θ),z)⋅r dV\iiint_E f(x, y, z) \, dV = \iiint_S f(r \cos(\theta), r \sin(\theta), z) \cdot r \, dV

It makes sense to change to cylindrical coordinates when we have symmetry around one axis.

Spherical coordinates

∭Ef(x,y,z) dV=∭Sf(ρsin⁡(φ)cos⁡(θ),ρsin⁡(φ)sin⁡(θ),ρcos⁡(φ))⋅ρ2sin⁡(φ) dV\iiint_E f(x, y, z) \, dV = \iiint_S f(\rho \sin(\varphi) \cos(\theta), \rho \sin(\varphi) \sin(\theta), \rho \cos(\varphi)) \cdot \rho^2 \sin(\varphi) \, dV

It makes sense to change to spherical coordinates when our solid is bounded by spheres and/or cones.

Computing mass of solid

Let EE be an arbitrary solid, with a density function, ρ(x,y,z)\rho(x, y, z)

We say that the mass of the solid is:

∭Eρ(x,y,z) dV\iiint_E \rho(x, y, z) \, dV

Center of Mass

One very important application is finding the center of mass of a solid.

Given a physical system with mim_i points, the center of mass has the coordinates, (x0,y0,z0)(x_0, y_0, z_0).

Therefore:

x0=∑mixi∑mi,y0=∑miyi∑mi,z0=∑mizi∑mi.x_0 = \dfrac{\sum m_i x_i}{\sum m_i}, \quad y_0 = \dfrac{\sum m_i y_i}{\sum m_i}, \quad z_0 = \dfrac{\sum m_i z_i}{\sum m_i}.

For an arbitrary solid, it’s almost the same:

x0=∭Eρ(x,y,z)⋅x dV∭Eρ(x,y,z) dV,y0=∭Eρ(x,y,z)⋅y dV∭Eρ(x,y,z) dV,z0=∭Eρ(x,y,z)⋅z dV∭Eρ(x,y,z) dV.\begin{align*} x_0 & = \dfrac{\iiint_E \rho(x, y, z) \cdot x \, dV}{\iiint_E \rho(x, y, z) \, dV}, \newline y_0 & = \dfrac{\iiint_E \rho(x, y, z) \cdot y \, dV}{\iiint_E \rho(x, y, z) \, dV}, \newline z_0 & = \dfrac{\iiint_E \rho(x, y, z) \cdot z \, dV}{\iiint_E \rho(x, y, z) \, dV}. \end{align*}

Parameterization over line

Given a line that passes through the point (x0,y0,z0)(x_0, y_0, z_0), with a direction of the vector, v⃗=⟨a,b,c⟩\vec{v} = \langle a, b, c \rangle.

If we want to parameterize this line, we can choose another point that this vector passes through as:

r⃗(t)=r⃗(t0)+tv⃗\vec{r}(t) = \vec{r}(t_0) + t\vec{v} (x(t),y(t),z(t))=(x0,y0,z0)+t(a,b,c)(x(t), y(t), z(t)) = (x_0, y_0, z_0) + t(a, b, c)

This means that:

x(t)=x0+ta,y(t)=y0+tb,z(t)=z0+tc.\begin{align*} x(t) & = x_0 + ta, \newline y(t) & = y_0 + tb, \newline z(t) & = z_0 + tc. \end{align*}

Line integral

A curve, CC, parameterized as r⃗(t)=⟨x(t),y(t)⟩\vec{r}(t) = \langle x(t), y(t) \rangle, for an interval t∈[a,b]t \in [a, b] and a continuous function, f:C→Rf: C \rarr \mathbb{R}.

Assuming x(t)x(t) and y(t)y(t) are differentiable.

∫Cf(x,y) ds=∫abf(x(t),y(t))x′(t)2+y′(t)2 dt\int_C f(x, y) \, ds = \int_a^b f(x(t), y(t)) \sqrt{x^\prime(t)^2 + y^\prime(t)^2} \, dt

Non-differentiable lines

There may be some cases where the parameterization isn’t differentiable.

Imagine we have a simple rectangular form. The four corners of the rectangle will not be differentiable.

What we can do is divide CC into nn subcurves.

C=C1∪C2∪…∪Cn,∫Cf(x,y) ds=∑j=1n∫Cjf(x,y) ds.\begin{align*} C & = C_1 \cup C_2 \cup \ldots \cup C_n, \newline \int_C f(x, y) \, ds & = \sum_{j = 1}^{n} \int_{C_j} f(x, y) \, ds. \end{align*}

Line integrals with respect to x or y

So far we have integrated with respect to the arc length. But we can integrate with respect to xx or yy.

∫Cf(x,y) dxor∫Cf(x,y) dy\int_C f(x, y) \, dx \quad \text{or} \quad \int_C f(x, y) \, dy ∫Cf(x,y) dx=∫abf(x(t),y(t))x′(t) dt,∫Cf(x,y) dy=∫abf(x(t),y(t))y′(t) dt.\begin{align*} \int_C f(x, y) \, dx & = \int_a^b f(x(t), y(t)) x^\prime(t) \, dt, \newline \int_C f(x, y) \, dy & = \int_a^b f(x(t), y(t)) y^\prime(t) \, dt. \end{align*}

Line integrals with three variables

There is no difference in two or three variables:

C⊂R3,f:C→R,r⃗(t)=⟨x(t),y(t),z(t)⟩,a≤t≤b.\begin{align*} & C \subset \mathbb{R}^3, \newline & f: C \rarr \mathbb{R}, \newline & \vec{r}(t) = \langle x(t), y(t), z(t) \rangle, \quad a \leq t \leq b. \end{align*} ∫Cf(x,y,z) ds=∫abf(x(t),y(t),z(t))x′(t)2+y′(t)2+z′(t)2 dt\int_C f(x, y, z) \, ds = \int_a^b f(x(t), y(t), z(t)) \sqrt{x^\prime(t)^2 + y^\prime(t)^2 + z^\prime(t)^2} \, dt

Vector field

A vector field is a function, FF:

F:D⊂R2→R2(2D),F:D⊂R3→R3(3D).\begin{align*} F & : D \subset \mathbb{R}^2 \rarr \mathbb{R}^2 \quad \text{(2D)}, \newline F & : D \subset \mathbb{R}^3 \rarr \mathbb{R}^3 \quad \text{(3D)}. \end{align*}

Gradient field

By this definition, we can say that.

Let f:D⊂R2→Rf: D \subset \mathbb{R}^2 \rarr \mathbb{R} be a differentiable function. The gradient is ∇f(x,y)=⟨fx(x,y),fy(x,y)⟩\nabla f(x, y) = \langle f_x(x, y), f_y(x, y) \rangle.

The gradient is therefore a vector field!

∇f:D→R2\nabla f: D \rarr \mathbb{R}^2

Conservative vector field

A vector field, FF, is called conservative, if there is a function, ff, for which ∇f=F\nabla f = F.

In this case, ff, is called a potential for FF.

Line integrals with vector fields

If CC is parameterized as r⃗(t)=⟨x(t),y(t),z(t)⟩\vec{r}(t) = \langle x(t), y(t), z(t) \rangle in the interval, a≤t≤ba \leq t \leq b. Then:

∫CF⋅dr=∫abF(x(t),y(t),z(t))⋅r′⃗(t) dt\int_C F \cdot dr = \int_a^b F(x(t), y(t), z(t)) \cdot \vec{r^\prime}(t) \, dt

Conservative vector field

Let D⊂R2D \subset \mathbb{R}^2 be open (every point in DD has a small disc around it, which contains DD), connected (consists of one single “piece”).

Let F:D→R2F: D \rarr \mathbb{R}^2 be a vector field. Then FF is conservative (there exists a ff such that ∇f=F\nabla f = F), if and only if:

∫CF⋅dr=0for every closed curve C⊂D.\int_C F \cdot dr = 0 \quad \text{for every closed curve } C \subset D.

NB: This only applies for R2\mathbb{R}^2.

Suppose F(x,y)=P(x,y)i⃗+Q(x,y)j⃗F(x, y) = P(x, y) \vec{i} + Q(x, y) \vec{j} is a conservative field. Then:

∂P∂y=∂Q∂x\dfrac{\partial P}{\partial y} = \dfrac{\partial Q}{\partial x}

Green’s Theorem

Let CC be a simple, closed curve oriented positively. Let DD be the region it surrounds and let P,Q:D→RP, Q: D \rarr \mathbb{R}.

∫CP dx+Q dy=∬D∂Q∂x−∂P∂y dx dy\int_C P \, dx + Q \, dy = \iint_D \dfrac{\partial Q}{\partial x} - \dfrac{\partial P}{\partial y} \, dx \, dy

Equivalently:

∫∂DP dx+Q dy=∬D∂Q∂x−∂P∂y dx dy\int_{\partial D} P \, dx + Q \, dy = \iint_D \dfrac{\partial Q}{\partial x} - \dfrac{\partial P}{\partial y} \, dx \, dy

Parametric surface

A parametric surface is a region, S⊂R3S \subset \mathbb{R}^3, which is the image of a function, r:D→R3r: D \rarr \mathbb{R}^3, defined on a region D⊂R2D \subset \mathbb{R}^2 of the plane.

Which means we can parameterize:

r⃗(u,v)=⟨x(u,v),y(u,v),z(u,v)⟩\vec{r}(u, v) = \langle x(u, v), y(u, v), z(u, v) \rangle

Tangent planes to surfaces.

Suppose SS is a parametric surface with parameterization r:D⊂R2→R3r: D \subset \mathbb{R}^2 \rarr \mathbb{R}^3.

r⃗(u,v)=x(u,v)i⃗+y(u,v)j⃗+z(u,v)k⃗\vec{r}(u, v) = x(u, v) \vec{i} + y(u, v) \vec{j} + z(u, v) \vec{k}

We define ru⃗(u,v)\vec{r_u}(u, v) as:

ru⃗=xu(u,v)i⃗+yu(u,v)j⃗+zu(u,v)k⃗\vec{r_u} = x_u(u, v) \vec{i} + y_u(u, v) \vec{j} + z_u(u, v) \vec{k}

And for the partial derivative of vv:

rv⃗=xv(u,v)i⃗+yv(u,v)j⃗+zv(u,v)k⃗\vec{r_v} = x_v(u, v) \vec{i} + y_v(u, v) \vec{j} + z_v(u, v) \vec{k}

The tangent plane, π\pi, to SS, at the point r(u0,v0)r(u_0, v_0) is the plane that contains ru(u0,v0)r_u(u_0, v_0) and rv(u0,v0)r_v(u_0, v_0).

Equivalently, it is the plane perpendicular to the cross product of ru(u0,v0)r_u(u_0, v_0) and rv(u0,v0)r_v(u_0, v_0), which goes through r(u0,v0)r(u_0, v_0).

Surface area

Let r:D→R3r: D \rarr \mathbb{R}^3 be a parameterization for a surface, SS.

Area(S)=∬D∣ru⃗×rv⃗∣ du dv.\text{Area}(S) = \iint_D | \vec{r_u} \times \vec{r_v} | \, du \, dv.

Surface integrals

Let r:D→R3r: D \rarr \mathbb{R}^3 be a parameterization of a surface, SS.

Let f:S→Rf: S \rarr \mathbb{R} be a function, then:

∬Sf(x,y,z) dS=∬Df(r⃗(u,v))∣ru⃗×rv⃗∣ du dv\iint_S f(x, y, z) \, dS = \iint_D f(\vec{r}(u, v)) | \vec{r_u} \times \vec{r_v} | \, du \, dv

Surface integrals over vector fields

Let SS be a parametric surface, parameterized by, r⃗:D→R3\vec{r}: D \rarr \mathbb{R}^3 and F:R3→R3F: \mathbb{R}^3 \rarr \mathbb{R}^3, be a vector field. Then:

∬SF⃗⋅dS=∬DF⃗(r⃗(u,v))⋅(ru⃗×rv⃗) du dv.\iint_S \vec{F} \cdot dS = \iint_D \vec{F}(\vec{r}(u, v)) \cdot (\vec{r_u} \times \vec{r_v}) \, du \, dv.

We call this the flux of F⃗\vec{F} through SS.

The Divergence Theorem

For a vector field, F⃗:R3→R3\vec{F}: \mathbb{R}^3 \rarr \mathbb{R}^3, the divergence is:

div⁡F⃗=∂P∂x+∂Q∂y+∂R∂z.\operatorname{div} \vec{F} = \dfrac{\partial P}{\partial x} + \dfrac{\partial Q}{\partial y} + \dfrac{\partial R}{\partial z}.

Let SS be a hollow surface and let EE be the 3-dimensional region it surrounds (∂E=S\partial E = S).

Then:

∬SF⃗⋅dS=∭Ediv⁡F⃗ dV.\iint_S \vec{F} \cdot dS = \iiint_E \operatorname{div} \vec{F} \, dV.

Equivalently:

∬∂EF⃗⋅dS=∭Ediv⁡F⃗ dV.\iint_{\partial E} \vec{F} \cdot dS = \iiint_E \operatorname{div} \vec{F} \, dV.

Stokes’ Theorem

So far we have seen Green’s Theorem as well as The Divergence theorem. But what is the reason that Green’s Theorem only works in R2\mathbb{R}^2?

Well, Stokes’ Theorem is essentially Green’s Theorem but in R3\mathbb{R}^3.

For F⃗:R3→R3\vec{F}: \mathbb{R}^3 \rarr \mathbb{R}^3, we define its curl as:

NB: it is also called rot and sometimes denoted as ∇×F⃗\nabla \times \vec{F}.

curl⁡F⃗=⟨∂R∂y−∂Q∂z,∂P∂z−∂R∂x,∂Q∂x−∂P∂y⟩.\operatorname{curl} \vec{F} = \left\langle \dfrac{\partial R}{\partial y} - \dfrac{\partial Q}{\partial z}, \dfrac{\partial P}{\partial z} - \dfrac{\partial R}{\partial x}, \dfrac{\partial Q}{\partial x} - \dfrac{\partial P}{\partial y} \right\rangle.

If S⊂R3S \subset \mathbb{R}^3 is a surface, surrounded by a simple, closed curve in R3\mathbb{R}^3. Then:

∫CF⃗⋅dr=∬Scurl⁡F⃗⋅dS.\int_C \vec{F} \cdot dr = \iint_S \operatorname{curl} \vec{F} \cdot dS.

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