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MATH 6AB Vector Calculus

Vector Calculus

Tue, Mar 17, 2026 13 min read

Multivariable Calculus

Vector

Arclength of a curve: L=∫ab(dxdt)2+(dydt)2dt=∫ab1+(dydx)2dxL = \int_{a}^{b} \sqrt{(\frac{dx}{dt})^2 + (\frac{dy}{dt})^2} dt = \int_{a}^{b} \sqrt{1 + (\frac{dy}{dx})^2} dx

c⃗(t)=p1⃗+t(p2⃗−p1⃗)\vec{c}(t) = \vec{p_1} + t(\vec{p_2} - \vec{p_1})

Dot Product

u⃗⋅v⃗=∣u⃗∣∣v⃗∣cos⁡θ\vec{u} \cdot \vec{v}= |\vec{u}||\vec{v}|\cos\theta
Parallel: u⃗⋅v⃗=∣u⃗∣∣v⃗∣\vec{u} \cdot \vec{v}= |\vec{u}||\vec{v}|.
Perpendicular: u⃗⋅v⃗=0\vec{u} \cdot \vec{v}= 0.

Cross Product

u⃗=⟨x1,y1,z1⟩v⃗=⟨x2,y2,z2⟩u⃗×v⃗=⟨y1z2−z1y2,z1x2−x1z2,x1y2−y1x2⟩∣u⃗×v⃗∣=∣u⃗∣∣v⃗∣sin⁡θ\vec{u} = \langle x_1, y_1, z_1 \rangle \\ \vec{v} = \langle x_2, y_2, z_2 \rangle \\ \vec{u} \times \vec{v} = \langle y_1z_2-z_1y_2, z_1x_2-x_1z_2, x_1y_2-y_1x_2 \rangle \\ |\vec{u} \times \vec{v}|= |\vec{u}||\vec{v}|\sin\theta The magnitude of the cross product is the area of a parallelogram formed by these two vectors.

Plane Equation

ax+by+cz=dax + by + cz = d
p⃗=w⃗+su⃗+tv⃗\vec{p} = \vec{w} + s\vec{u} + t\vec{v}

Parallel with: ax+by+cz=0ax + by + cz = 0
p⃗=su⃗+tv⃗\vec{p} = s\vec{u} + t\vec{v}

Move by ⟨2,3,4⟩\langle 2, 3, 4 \rangle
p⃗=⟨2,3,4⟩+w⃗+su⃗+tv⃗\vec{p} = \langle 2, 3, 4 \rangle + \vec{w} + s\vec{u} + t\vec{v}
a(x−2)+b(y−3)+c(z−4)=da(x - 2) + b(y - 3) + c(z - 4) = d

Perpendicular: n⃗=⟨a,b,c⟩\vec{n} = \langle a, b, c \rangle.
n⃗=u⃗×v⃗\vec{n} = \vec{u} \times \vec{v}.
n⃗=∇f=fr×fθ\vec{n} = \nabla f = f_r \times f_\theta.

Two planes are parallel when their normal vectors are parallel.

Derivatives

v⃗(t)′=⟨x⃗(t)′,y⃗(t)′,z⃗(t)′⟩\vec{v}(t)' = \langle \vec{x}(t)', \vec{y}(t)', \vec{z}(t)' \rangle.
∫v⃗(t)=⟨∫x⃗(t),∫y⃗(t),∫z⃗(t)⟩\int\vec{v}(t) = \langle \int\vec{x}(t), \int\vec{y}(t), \int\vec{z}(t) \rangle.
(u⃗⋅v⃗)′=u⃗′⋅v⃗+u⃗⋅v⃗′(\vec{u}\cdot \vec{v})' = \vec{u}'\cdot \vec{v} + \vec{u}\cdot \vec{v}'.

Curvature: κ(t)=∣v⃗(t)′×v⃗(t)′′∣∣v⃗(t)′∣3\kappa(t) = \frac{|\vec{v}(t)' \times \vec{v}(t)''|}{|\vec{v}(t)'|^3}

Arc-length parameterization s(t)=∫t0t∣r⃗(u)′∣du t=t(s)s(t) = \int_{t_0}^t |\vec{r}(u)'|du \ \\ t = t(s).
Replace tt with t(s)t(s), r⃗(t)\vec{r}(t) -> r⃗(t(s))=r⃗(s)\vec{r}(t(s)) = \vec{r}(s); r⃗(s)′=1\vec{r}(s)' = 1.
Curvature is the same as acceleration.

Partial Derivatives

Clairaut's Theorem: The mixed partials with different orders are equal: fxy=fyxf_{xy} = f_{yx}

(fg)′′′′=f′′′′g+4f′′′g′+6f′′g′′+4f′g′′′+fg′′′′(fg)'''' = f''''g + 4f'''g' + 6f''g'' + 4f'g''' + fg''''

dfdt=dfdx⋅dxdt+dfdy⋅dydt+dfdz⋅dzdt\frac{df}{dt} = \frac{df}{dx}\cdot \frac{dx}{dt} + \frac{df}{dy}\cdot \frac{dy}{dt} + \frac{df}{dz}\cdot \frac{dz}{dt}

F(x,y,z)=0dFdy⋅dydz+dFdz=0dydz=−FzFyF(x, y, z) = 0 \\ \frac{dF}{dy}\cdot \frac{dy}{dz} + \frac{dF}{dz} = 0 \\ \frac{dy}{dz} = -\frac{F_z}{F_y} \\

f(x,y),x(u,v),y(u,v)f(x, y), x(u, v), y(u, v) [fufv]=[fxfy][xuxvyuyv]\begin{bmatrix} f_u & f_v \end{bmatrix} = \begin{bmatrix} f_x & f_y \end{bmatrix} \begin{bmatrix} x_u & x_v \\ y_u & y_v \\ \end{bmatrix}

Optimization

Gradient vector: ∇f(x,y)=⟨fx,fy⟩\nabla f(x, y) = \langle f_x, f_y \rangle.
Movement vector: v⃗=⟨dx,dy⟩\vec{v} = \langle dx, dy \rangle.

Tangent Plane

dz=fxdx+fydy=∇f⋅v⃗dz = f_xdx + f_ydy = \nabla f\cdot \vec{v}.
Δz≈fxΔx+fyΔy\Delta z \approx f_x\Delta x + f_y\Delta y.
z=z0+fx(x−x0)+fy(y−y0)z = z_0 + f_x(x - x_0) + f_y(y - y_0).

Directional Derivative

Slope=riserun=∇f⋅v⃗∣v⃗∣=∇f⋅u⃗=∣∇f∣∣u⃗∣cos⁡θSlope = \frac{rise}{run} = \frac{\nabla f\cdot \vec{v}}{|\vec{v}|} = \nabla f \cdot \vec{u} = |\nabla f||\vec{u}| \cos\theta

Movement in the direction of the gradient has a maximum slope equal to the magnitude of the gradient. Movement perpendicular to the gradient has a slope of 0.

Critical Points

f(x,y)f(x, y), ∇f=0\nabla f = 0

Second Derivative Test D(x0,y0)=∣fxxfxyfyxfyy∣=fxxfyy−fxy2D(x_0, y_0) = \begin{vmatrix} f_{xx} & f_{xy} \\ f_{yx} & f_{yy} \\ \end{vmatrix} = f_{xx}f_{yy} - {f_{xy}}^2 D>0,fxx>0D > 0, f_{xx} > 0, relative minimum; D>0,fxx<0D > 0, f_{xx} < 0, relative maximum; D<0D < 0, saddle point; D=0D = 0, don't know.

Lagrange Multipliers

Constraint function: g(x,y)=0g(x, y) = 0 ∇f=λ∇g\nabla f = \lambda \nabla g fx=λgxfy=λgyg(x,y)=0f_x = \lambda g_x \\ f_y = \lambda g_y \\ g(x, y) = 0

Double Integrals

Over rectangular region R=[a,b]×[c,d]R = [a, b] \times [c, d], a Cartesian product of intervals.

Definition: ∫∫Rf(x,y)dA,∫∫Rf(x,y)dx dy\int\int_R f(x, y) dA, \int\int_R f(x, y) dx\ dy

Cavalieri's Principle (the slice method): Volume=∫abA(x)dx\text{Volume} = \int_a^b A(x) dx, where A(x)A(x) is the area of the cross section at xx.
Therefore, we have,

∫∫Rf(x,y)dA=∫ab(∫cdf(x,y)dy)dx=∫cd(∫abf(x,y)dx)dy\begin{aligned} \int\int_R f(x, y) dA &= \int_a^b \left( \int_c^d f(x, y) dy \right) dx \\ &= \int_c^d \left( \int_a^b f(x, y) dx \right) dy \\ \end{aligned}

Fubini's Theorem: If ff is continuous on a rectangular region RR, then ∫∫Rf(x,y)dA=∫ab∫cdf(x,y)dy dx=∫cd∫abf(x,y)dx dy\int\int_R f(x, y) dA = \int_a^b \int_c^d f(x, y) dy\ dx = \int_c^d \int_a^b f(x, y) dx\ dy

If f(x,y)=g(x)h(y)f(x, y) = g(x)h(y), then ∫∫Rf(x,y)dA=(∫abg(x)dx)(∫cdh(y)dy)\int\int_R f(x, y) dA = \left( \int_a^b g(x) dx \right) \left( \int_c^d h(y) dy \right)

Properties:

  1. Any continuous function defined on a closed rectangle RR is integrable.
  2. If the set of discontinuities lies on a finite union of graphs of continuous functions, then ff is integrable on RR.

Mean Value Theorem for Double Integrals: If ff is continuous on a closed, bounded region RR with area AA, then there exists a point (x0,y0)(x_0, y_0) in RR such that ∫∫Rf(x,y)dA=f(x0,y0)⋅A(R)\int\int_R f(x, y) dA = f(x_0, y_0) \cdot A(R)

Theorems

∫abd−c dx=∫ab∫cd1dydx\int_a^b d - c\ dx = \int_a^b \int_c^d 1 dydx, then ∫ab∫cdf(x,y) dydx\int_a^b \int_c^d f(x, y)\ dydx.
Estimating: If g≤f≤hg \le f \le h, then ∫∫RgdA≤∫∫RfdA≤∫∫RhdA\int\int_R g dA \le \int\int_R f dA \le \int\int_R h dA

Change of Coordinates

Double Integral

(x,y)→(u,v)(x, y) \to (u, v) where x=fx(u,v)x = f_x(u, v) and y=fy(u,v)y = f_y(u, v)

Jacobian Determinant:

J=∂(x,y)∂(u,v)=∣∂x∂u∂x∂v∂y∂u∂y∂v∣=∂x∂u⋅∂y∂v−∂x∂v⋅∂y∂uJ = \frac{\partial(x, y)}{\partial(u, v)} = \begin{vmatrix} \frac{\partial x}{\partial u} & \frac{\partial x}{\partial v} \\ \frac{\partial y}{\partial u} & \frac{\partial y}{\partial v} \\ \end{vmatrix} = \frac{\partial x}{\partial u} \cdot \frac{\partial y}{\partial v} - \frac{\partial x}{\partial v} \cdot \frac{\partial y}{\partial u}

The change of variables formula is: ∫∫Rf(x,y) dxdy=∫∫Sf(fx(u,v),fy(u,v))∣∂(x,y)∂(u,v)∣dudv\int\int_R f(x, y)\ dx dy = \int\int_S f(f_x(u, v), f_y(u, v)) \left| \frac{\partial(x, y)}{\partial(u, v)} \right| du dv

Triple Integral

(x,y,z)→(u,v,w)(x, y, z) \to (u, v, w) where x=fx(u,v,w)x = f_x(u, v, w), y=fy(u,v,w)y = f_y(u, v, w), and z=fz(u,v,w)z = f_z(u, v, w)

Jacobian Determinant:

J=∂(x,y,z)∂(u,v,w)=∣∂x∂u∂x∂v∂x∂w∂y∂u∂y∂v∂y∂w∂z∂u∂z∂v∂z∂w∣J = \frac{\partial(x, y, z)}{\partial(u, v, w)} = \begin{vmatrix} \frac{\partial x}{\partial u} & \frac{\partial x}{\partial v} & \frac{\partial x}{\partial w} \\ \frac{\partial y}{\partial u} & \frac{\partial y}{\partial v} & \frac{\partial y}{\partial w} \\ \frac{\partial z}{\partial u} & \frac{\partial z}{\partial v} & \frac{\partial z}{\partial w} \\ \end{vmatrix}

The change of variables formula is: ∫∫∫Rf(x,y,z) dxdydz=∫∫∫Sf(fx,fy,fz)∣∂(x,y,z)∂(u,v,w)∣dudvdw\int\int\int_R f(x, y, z)\ dx dy dz = \int\int\int_S f(f_x, f_y, f_z) \left| \frac{\partial(x, y, z)}{\partial(u, v, w)} \right| du dv dw

The Gaussian integral: ∫−∞∞e−x2dx=π\int_{-\infty}^{\infty} e^{-x^2} dx = \sqrt{\pi}

Typical Coordinate Systems

Polar Coordinate (r,θ)(r, \theta)

(x,y)=(rcos⁡θ,rsin⁡θ)(x, y) = (r\cos\theta, r\sin\theta), ∂(x,y)∂(r,θ)=r\frac{ \partial(x, y) }{ \partial(r, \theta) } = r

∫02π∫0Rf(r,θ)r drdθ\int_0^{2\pi}\int_0^R f(r, \theta) r\ dr d\theta

Ellipse

(xa)2+(yb)2=R2(\frac{x}{a})^2 + (\frac{y}{b})^2 = R^2

(x,y)=(arcos⁡θ,brsin⁡θ)(x, y) = (ar\cos\theta, br\sin\theta), ∂(x,y)∂(r,θ)=abr\frac{ \partial(x, y) }{ \partial(r, \theta) } = abr

∫02π∫0Rf(r,θ)abr drdθ\int_0^{2\pi}\int_0^R f(r, \theta) abr\ dr d\theta

Cylindrical Coordinate (r,θ,z)(r, \theta, z)

(x,y,z)=(rcos⁡θ,rsin⁡θ,z)(x, y, z) = (r\cos\theta, r\sin\theta, z), ∂(x,y,z)∂(r,θ,z)=r\frac{ \partial(x, y, z) }{ \partial(r, \theta, z) } = r

∫z0z1∫02π∫0Rf(r,θ,z)r drdθdz\int_{z_0}^{z_1}\int_0^{2\pi}\int_0^R f(r, \theta, z) r \ dr d\theta dz

Spherical Coordinate (r,θ,ϕ)(r, \theta, \phi)

(x,y,z)=(rsin⁡ϕcos⁡θ,rsin⁡ϕsin⁡θ,rcos⁡ϕ)(x, y, z) = (r\sin\phi\cos\theta, r\sin\phi\sin\theta, r\cos\phi), ∂(x,y,z)∂(r,θ,ϕ)=r2sin⁡ϕ\frac{ \partial(x, y, z) }{ \partial(r, \theta, \phi) } = r^2\sin\phi

∫0π∫02π∫0Rf(r,θ,ϕ)r2sin⁡ϕ drdθdϕ\int_0^{\pi}\int_0^{2\pi}\int_0^R f(r, \theta, \phi) r^2\sin\phi\ dr d\theta d\phi

Line Integral (Path Integral)

Definition: Integrals over curves.

r⃗(t)=⟨x(t),y(t)⟩,a≤t≤bC\vec{r}(t) = \langle x(t), y(t) \rangle, a \le t \le b \\ C is the curve parameterized by r⃗(t)\vec{r}(t)

ds=∣r⃗(t)′∣dtdr⃗=r⃗(t)′dtds = |\vec{r}(t)'| dt \\ d\vec{r} = \vec{r}(t)' dt ∫Cf(x,y)ds=∫abf(r⃗(t))∣r⃗(t)′∣dt\int_C f(x, y) ds = \int_a^b f(\vec{r}(t)) |\vec{r}(t)'| dt ∫CF⃗⋅dr⃗=∫abF⃗(r⃗(t))⋅r⃗(t)′dt\int_C \vec{F} \cdot d\vec{r} = \int_a^b \vec{F}(\vec{r}(t)) \cdot \vec{r}(t)' dt

r⃗(t)=⟨x(t),y(t)⟩,f(x,y)\vec{r}(t) = \langle x(t), y(t) \rangle, f(x, y).
∫abf(r⃗(t))∣r⃗(t)′∣dt\int_a^b f(\vec{r}(t))|\vec{r}(t)'|dt

F⃗(x,y)=⟨P(x,y),Q(x,y)⟩\vec{F}(x, y) = \langle P(x, y), Q(x, y) \rangle.
∫abF⃗(r⃗(t))⋅r⃗(t)′dt\int_a^b \vec{F}(\vec{r}(t)) \cdot \vec{r}(t)'dt

TT is the unit tangent vector to CC at the point r⃗(t)\vec{r}(t). T⃗=r⃗(t)′∣r⃗(t)′∣\vec{T} = \frac{\vec{r}(t)'}{|\vec{r}(t)'|}

Reparameterization

If CC is parameterized by r⃗(t),a≤t≤b\vec{r}(t), a \le t \le b and also by p⃗(s),c≤s≤d\vec{p}(s), c \le s \le d, where r⃗(t)=p⃗(g(t))\vec{r}(t) = \vec{p}(g(t)) for some differentiable function g(t)g(t) with g(a)=cg(a) = c and g(b)=dg(b) = d, then ∫Cf(x,y)ds=∫abf(r⃗(t))∣r⃗(t)′∣dt=∫cdf(p⃗(s))∣p⃗(s)′∣ds\int_C f(x, y) ds = \int_a^b f(\vec{r}(t)) |\vec{r}(t)'| dt = \int_c^d f(\vec{p}(s)) |\vec{p}(s)'| ds ∫CF⃗⋅dr⃗=∫abF⃗(r⃗(t))⋅r⃗(t)′dt=∫cdF⃗(p⃗(s))⋅p⃗(s)′ds\int_C \vec{F} \cdot d\vec{r} = \int_a^b \vec{F}(\vec{r}(t)) \cdot \vec{r}(t)' dt = \int_c^d \vec{F}(\vec{p}(s)) \cdot \vec{p}(s)' ds

Line Integrals of Gradient Fields

If F⃗=∇f\vec{F} = \nabla f, then ∫CF⃗⋅dr⃗=f(r⃗(b))−f(r⃗(a))\int_C \vec{F} \cdot d\vec{r} = f(\vec{r}(b)) - f(\vec{r}(a))

Images

Let A be a matrix with det and let be the linear mapping of to given by (matrix multiplication). Then transforms parallelograms into parallelograms and vertices into vertices. Moreover, if is a parallelogram, must be a parallelogram.

A linear transformation matrix AA is one-to-one and onto if and only if det⁡(A)≠0\det(A) \neq 0.

TT maps [0,1]×[0,1][0, 1] \times [0, 1] to the parallelogram spanned by the vectors ⟨a,c⟩\langle a, c \rangle and ⟨b,d⟩\langle b, d \rangle. T(u,v)=⟨au+bv,cu+dv⟩T(u, v) = \langle au + bv, cu + dv \rangle. The area of the parallelogram is ∣det⁡(A)∣=∣ad−bc∣|\det(A)| = |ad - bc|.

Applications

Average Value

The average value of ff over a region RR is given by favg=∫∫Rf(x,y)dxdy∫∫Rdxdyf_{avg} = \frac{\int\int_R f(x, y) dx dy}{\int\int_R dx dy}

Center of Mass

The total mass MM of a lamina with density function δ(x,y)\delta(x, y) over a region RR is given by M=∫∫Rδ(x,y)dAM = \int\int_R \delta(x, y) dA

The center of mass (xˉ,yˉ)(\bar{x}, \bar{y}) of a lamina with density function δ(x,y)\delta(x, y) over a region RR is given by xˉ=∫∫Rxδ(x,y)dAM,yˉ=∫∫Ryδ(x,y)dAM\bar{x} = \frac{\int\int_R x \delta(x, y) dA}{M}, \quad \bar{y} = \frac{\int\int_R y \delta(x, y) dA}{M}

Moment of Inertia

Moments of inertia about the coordinate axes with uniform density δ\delta are given by Ix=δ∫∫∫R(y2+z2)dV,Iy=δ∫∫∫R(x2+z2)dV,Iz=δ∫∫∫R(x2+y2)dVI_x = \delta \int\int\int_R (y^2 + z^2) dV, \quad I_y = \delta \int\int\int_R (x^2 + z^2) dV, \quad I_z = \delta \int\int\int_R (x^2 + y^2) dV

Gravitational Force

The gravitational force exerted on a point mass mm located at the point (x0,y0,z0)(x_0, y_0, z_0) by a solid region RR with density function δ(x,y,z)\delta(x, y, z) is given by F⃗=Gm∫∫∫Rδ(x,y,z)r2r^dV\vec{F} = Gm \int\int\int_R \frac{\delta(x, y, z)}{r^2} \hat{r} dV ∣F∣=Gm∫∫∫Rδ(x,y,z)rdV|F| = Gm \int\int\int_R \frac{\delta(x, y, z)}{r} dV where GG is the gravitational constant, rr is the distance from the point mass to the point (x,y,z)(x, y, z), and r^\hat{r} is the unit vector pointing from (x,y,z)(x, y, z) to (x0,y0,z0)(x_0, y_0, z_0).

Isaac Newton's Breathtaking Proposition 71

A uniform spherical shell of mass MM exerts a gravitational force on a point mass mm located outside the shell as if all the shell's mass were concentrated at its center. If the point mass is located inside the shell, the net gravitational force exerted on it by the shell is zero.

Surface Integral

A parameterization of a surface SS is a vector function 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 defined on a region RR in the uvuv-plane such that r⃗\vec{r} is one-to-one and r⃗(R)=S\vec{r}(R) = S.

Tu=r⃗u=∂r⃗∂uT_u = \vec{r}_u = \frac{\partial \vec{r}}{\partial u} and Tv=r⃗v=∂r⃗∂vT_v = \vec{r}_v = \frac{\partial \vec{r}}{\partial v} are tangent vectors to the surface, and n⃗=r⃗u×r⃗v∣r⃗u×r⃗v∣\vec{n} = \frac{\vec{r}_u \times \vec{r}_v}{|\vec{r}_u \times \vec{r}_v|} is the unit normal vector to the surface. The magnitude of the cross product ∣r⃗u×r⃗v∣|\vec{r}_u \times \vec{r}_v| gives the area of the parallelogram spanned by the tangent vectors, which is used to compute the surface area element dSdS.

An equation of the tangent plane to the surface at a point r⃗(u0,v0)\vec{r}(u_0, v_0) is given by n⃗⋅(r⃗−r⃗(u0,v0))=0\vec{n} \cdot (\vec{r} - \vec{r}(u_0, v_0)) = 0 n1(x−x0)+n2(y−y0)+n3(z−z0)=0n_1(x - x_0) + n_2(y - y_0) + n_3(z - z_0) = 0

The surface SS is regular if Tu×Tv≠0⃗T_u \times T_v \neq \vec{0} for all (u,v)(u, v) in RR. This condition ensures that the surface does not have any singularities or self-intersections, allowing for a well-defined normal vector and surface area element.

Surface area of SS is given by

A(S)=∬R∣r⃗u×r⃗v∣dudv=∬R(∂(y,z)∂(u,v))2+(∂(z,x)∂(u,v))2+(∂(x,y)∂(u,v))2 dudvA(S) = \iint_R |\vec{r}_u \times \vec{r}_v| du dv \\ = \iint_R \sqrt{\left( \frac{\partial(y, z)}{\partial(u, v)} \right)^2 + \left( \frac{\partial(z, x)}{\partial(u, v)} \right)^2 + \left( \frac{\partial(x, y)}{\partial(u, v)} \right)^2} \, du dv

Parametic equation of a surface: ax+by+cz=dax + by + cz = d r⃗(u,v)=w⃗+su⃗+tv⃗\vec{r}(u, v) = \vec{w} + s\vec{u} + t\vec{v} Parametic surface integral: ∬Sf(x,y,z)dS=∬Rf(r⃗(u,v))∣r⃗u×r⃗v∣dudv\iint_S f(x, y, z) dS = \iint_R f(\vec{r}(u, v)) |\vec{r}_u \times \vec{r}_v| du dv Vector field surface integral: ∬SF⃗⋅dS⃗=∬RF⃗(r⃗(u,v))⋅(r⃗u×r⃗v)dudv\iint_S \vec{F} \cdot d\vec{S} = \iint_R \vec{F}(\vec{r}(u, v)) \cdot (\vec{r}_u \times \vec{r}_v) du dv

dS⃗=(r⃗u×r⃗v)dudvd\vec{S} = (\vec{r}_u \times \vec{r}_v) du dv

How to find the parameterization of a surface defined by an implicit equation f(x,y,z)=0f(x, y, z) = 0?

  1. Find the normal vector n⃗=∇f=⟨∂f∂x,∂f∂y,∂f∂z⟩\vec{n} = \nabla f = \langle \frac{\partial f}{\partial x}, \frac{\partial f}{\partial y}, \frac{\partial f}{\partial z} \rangle.
  2. Find two tangent vectors u⃗\vec{u} and v⃗\vec{v} such that n⃗⋅u⃗=0\vec{n} \cdot \vec{u} = 0 and n⃗⋅v⃗=0\vec{n} \cdot \vec{v} = 0.
  3. Find a point w⃗\vec{w} on the surface.
  4. The parameterization is given by r⃗(s,t)=w⃗+su⃗+tv⃗\vec{r}(s, t) = \vec{w} + s\vec{u} + t\vec{v}.

Area of a surface defined by f(x,y,z)=0f(x, y, z) = 0 is given by A(S)=∬R∣∇f∣∣∇f⋅k⃗∣dudvA(S) = \iint_R \frac{|\nabla f|}{|\nabla f \cdot \vec{k}|} du dv where k⃗\vec{k} is the unit vector in the zz-direction. This formula arises from the fact that the area element dSdS can be expressed in terms of the gradient of ff and the projection of the surface onto the xyxy-plane. The term ∣∇f∣|\nabla f| accounts for the rate of change of the surface, while ∣∇f⋅k⃗∣|\nabla f \cdot \vec{k}| accounts for the angle between the surface and the xyxy-plane, ensuring that the area is correctly scaled based on the orientation of the surface. A=∬R1+(∂z∂x)2+(∂z∂y)2dxdyA = \iint_R \sqrt{1 + \left( \frac{\partial z}{\partial x} \right)^2 + \left( \frac{\partial z}{\partial y} \right)^2} dx dy

For rotation about the zz-axis, the surface area is given by A=∬R2πx2+y21+(∂z∂x)2+(∂z∂y)2dxdyA = \iint_R 2\pi \sqrt{x^2 + y^2} \sqrt{1 + \left( \frac{\partial z}{\partial x} \right)^2 + \left( \frac{\partial z}{\partial y} \right)^2} dx dy

For rotation about the yy-axis, the surface area is given by A=∬R2πx1+(∂y∂x)2dxA = \iint_R 2\pi x \sqrt{1 + \left( \frac{\partial y}{\partial x} \right)^2} dx

Graph

If z=f(x,y)z = f(x, y), then ∣ru×rv∣=1+(∂z∂x)2+(∂z∂y)2|r_u \times r_v| = \sqrt{1 + \left( \frac{\partial z}{\partial x} \right)^2 + \left( \frac{\partial z}{\partial y} \right)^2}

Sphere

dS=r2sin⁡ϕ dϕdθdS = r^2\sin\phi\ d\phi d\theta

Green's Theorem

A simple closed curve CC has two orientations:

  • Counterclockwise orientation (positive orientation), C+C^+
  • Clockwise orientation (negative orientation), C−C^-

∫CF⃗⋅dr⃗=∬R(∂Q∂x−∂P∂y)dA\int_C \vec{F} \cdot d\vec{r} = \iint_R \left( \frac{\partial Q}{\partial x} - \frac{\partial P}{\partial y} \right) dA

Lemma

Lemma 1. Let DD be a yy-simple region and let CC be its boundary. Suppose P:D→RP: D \to \mathbb{R} is of class C1C^1. Then

∫C+P dx=−∬D∂P∂y dx dy\int_{C^+} P \, dx = - \iint_D \frac{\partial P}{\partial y} \, dx \, dy

(The left-hand side denotes the line integral ∫C+P dx+Q dy\int_{C^+} P \, dx + Q \, dy, where Q=0Q = 0.)

Lemma 2. Let DD be an xx-simple region and let CC be its boundary. Suppose Q:D→RQ: D \to \mathbb{R} is of class C1C^1. Then

∫C+Q dy=∬D∂Q∂x dx dy\int_{C^+} Q \, dy = \iint_D \frac{\partial Q}{\partial x} \, dx \, dy

(The left-hand side denotes the line integral ∫C+P dx+Q dy\int_{C^+} P \, dx + Q \, dy, where P=0P = 0.)

Theorems

Theorem 1: Suppose DD is a simple region and CC is its boundary, and P:D→RP: D \to \mathbb{R} and Q:D→RQ: D \to \mathbb{R} are of class C1C^1. Then ∫C+P dx+Q dy=∬D(∂Q∂x−∂P∂y)dxdy\int_{C^+} P \, dx + Q \, dy = \iint_D \left( \frac{\partial Q}{\partial x} - \frac{\partial P}{\partial y} \right) dx dy ∫C−P dx+Q dy=−∬D(∂Q∂x−∂P∂y)dxdy\int_{C^-} P \, dx + Q \, dy = - \iint_D \left( \frac{\partial Q}{\partial x} - \frac{\partial P}{\partial y} \right) dx dy

Theorem 2: Area via Green's Theorem. If CC is a simple closed curve that bounds a region to which Green's theorem applies, then the area of the region DD bounded by C=∂DC = \partial D is A=12∮∂D(x dy−y dx)A = \frac{1}{2} \oint_{\partial D} \left( x \, dy - y \, dx \right)

Theorem 3: Vector Form of Green's Theorem. Let D⊂R2D \subset \mathbb{R}^2 be a region to which Green's theorem applies, let ∂D\partial D be its (positively oriented) boundary, and let F=Pi+Qj\mathbf{F} = P\mathbf{i} + Q\mathbf{j} be a C1C^1 vector field on DD. Then ∮∂DF⋅ds=∬D(curl⁡F)⋅k dA=∬D(∇×F)⋅k dA\oint_{\partial D} \mathbf{F} \cdot d\mathbf{s} = \iint_D (\operatorname{curl}\mathbf{F}) \cdot \mathbf{k} \, dA = \iint_D (\nabla \times \mathbf{F}) \cdot \mathbf{k} \, dA

Theorem 4: Divergence Theorem in the Plane. Let D⊂R2D \subset \mathbb{R}^2 be a region to which Green's theorem applies and let ∂D\partial D be its boundary. Let n\mathbf{n} denote the outward unit normal to ∂D\partial D. If c:[a,b]→R2\mathbf{c} : [a, b] \to \mathbb{R}^2, t↦c(t)=(x(t),y(t))t \mapsto \mathbf{c}(t) = (x(t), y(t)) is a positively oriented parametrization of ∂D\partial D, then n\mathbf{n} is given by n=(y′(t),−x′(t))[x′(t)]2+[y′(t)]2\mathbf{n} = \frac{(y'(t), -x'(t))}{\sqrt{[x'(t)]^2 + [y'(t)]^2}} (see Figure 18.9). Let F=Pi+Qj\mathbf{F} = P\mathbf{i} + Q\mathbf{j} be a C1C^1 vector field on DD. Then ∮∂DF⋅n ds=∬Ddiv⁡F dA\oint_{\partial D} \mathbf{F} \cdot \mathbf{n} \, ds = \iint_D \operatorname{div} \mathbf{F} \, dA

Stokes' Theorem

div: div F⃗=∇⋅F⃗=∂Fx∂x+∂Fy∂y+∂Fz∂z\text{div } \vec{F} = \nabla \cdot \vec{F} = \frac{\partial F_x}{\partial x} + \frac{\partial F_y}{\partial y} + \frac{\partial F_z}{\partial z}.
curl: curl F⃗=∇×F⃗=⟨∂∂yFz−∂∂zFy,∂∂zFx−∂∂xFz,∂∂xFy−∂∂yFx⟩\text{curl } \vec{F} = \nabla \times \vec{F} = \langle \frac{\partial }{\partial y}F_z - \frac{\partial }{\partial z}F_y, \frac{\partial }{\partial z}F_x - \frac{\partial }{\partial x}F_z, \frac{\partial }{\partial x}F_y - \frac{\partial }{\partial y}F_x \rangle.
flux: ∬SF⃗⋅dS⃗=∬SF⃗⋅n⃗dS\iint_S \vec{F} \cdot d\vec{S} = \iint_S \vec{F} \cdot \vec{n} dS.
flux of curl: ∬S(∇×F⃗)⋅dS⃗\iint_S (\nabla \times \vec{F}) \cdot d\vec{S}.

n⃗=r⃗u×r⃗v∣r⃗u×r⃗v∣\vec{n} = \frac{\vec{r}_u \times \vec{r}_v}{|\vec{r}_u \times \vec{r}_v|} is the unit normal vector to the surface.

Stokes' Theorem for Graph

∫∂SF⃗⋅dr⃗=∬S(∇×F⃗)⋅dS⃗=∬Scurl (F⃗)⋅n⃗dA\int_{\partial S} \vec{F} \cdot d\vec{r} = \iint_S (\nabla \times \vec{F}) \cdot d\vec{S} = \iint_S \text{curl } (\vec{F}) \cdot \vec{n} dA

Stokes' Theorem for Parametrized Surface

∬S(∇×F⃗)⋅dS⃗=∫∂SF⃗⋅dr⃗\iint_S (\nabla \times \vec{F}) \cdot d\vec{S} = \int_{\partial S} \vec{F} \cdot d\vec{r}

Conservative Vector Fields

If F⃗=∇f\vec{F} = \nabla f, then ∫SF⃗⋅dr⃗=f(r⃗(b))−f(r⃗(a))\int_{S} \vec{F} \cdot d\vec{r} = f(\vec{r}(b)) - f(\vec{r}(a)).

Theorem 1: Conservative Fields. Let F⃗\vec{F} be a C1C^1 vector field defined on R3\mathbb{R}^3, except possibly for a finite number of points. The following conditions on F⃗\vec{F} are all equivalent:

  1. For any oriented simple closed curve CC, ∫CF⃗⋅ds⃗=0\displaystyle \int_C \vec{F} \cdot d\vec{s} = 0.
  2. For any two oriented simple curves C1C_1 and C2C_2 that have the same endpoints, ∫C1F⃗⋅ds⃗=∫C2F⃗⋅ds⃗\displaystyle \int_{C_1} \vec{F} \cdot d\vec{s} = \int_{C_2} \vec{F} \cdot d\vec{s}.
  3. F⃗\vec{F} is the gradient of some function ff; that is, F⃗=∇f\vec{F} = \nabla f (and if F⃗\vec{F} has one or more exceptional points where it fails to be defined, ff is also undefined there).
  4. ∇×F⃗=0⃗\nabla \times \vec{F} = \vec{0}.

A vector field satisfying one (and, hence, all) of the conditions 1–4 is called a conservative vector field.

Corollary 1: If F⃗\vec{F} is a C1C^1 vector field on R2\mathbb{R}^2 of the form Pi⃗+Qj⃗P\vec{i} + Q\vec{j} that satisfies ∂P∂y=∂Q∂x\displaystyle \frac{\partial P}{\partial y} = \frac{\partial Q}{\partial x}, then F⃗=∇f\vec{F} = \nabla f for some ff on R2\mathbb{R}^2.

Theorem 2: If F⃗\vec{F} is a C1C^1 vector field on all of R3\mathbb{R}^3 with ∇⋅F⃗=0\nabla \cdot \vec{F} = 0, then there exists a C1C^1 vector field G⃗\vec{G} with F⃗=∇×G⃗\vec{F} = \nabla \times \vec{G}.

If FF has a potential function ff, then it satisfies the cross-partial property: ∂Fx∂y=∂Fy∂x\frac{\partial F_x}{\partial y} = \frac{\partial F_y}{\partial x}.

Gauss' Theorem

Gauss' Divergence Theorem

Let WW be a symmetric elementary region in space. ∭W(∇⋅F⃗)dV=∬∂WF⃗⋅dS⃗\iiint_W (\nabla \cdot \vec{F}) dV = \iint_{\partial W} \vec{F} \cdot d\vec{S} ∭W(div F⃗)dV=∬∂W(F⃗⋅n⃗)dS\iiint_W (\text{div } \vec{F}) dV = \iint_{\partial W} (\vec{F} \cdot \vec{n}) dS

Gauss' Law

Let MM be a symmetric elementary region in R3\mathbb{R}^3. If (0,0,0)∉∂M(0, 0, 0) \notin \partial M, then

∬∂Mr⃗⋅n⃗r3 dS={4π,if (0,0,0)∈M,0,if (0,0,0)∉M.\iint_{\partial M} \frac{\vec{r} \cdot \vec{n}}{r^3} \, dS = \begin{cases} 4\pi, & \text{if } (0, 0, 0) \in M, \\ 0, & \text{if } (0, 0, 0) \notin M. \end{cases}

where

r⃗(x,y,z)=xi⃗+yj⃗+zk⃗,r(x,y,z)=∥r⃗(x,y,z)∥=x2+y2+z2.\vec{r}(x, y, z) = x\vec{i} + y\vec{j} + z\vec{k}, \\ r(x, y, z) = \|\vec{r}(x, y, z)\| = \sqrt{x^2 + y^2 + z^2}.
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