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An overview of various methods for calculating integrals, including direct techniques for definite integrals, line integrals, iterated integrals, and double or triple integrals, as well as indirect techniques using gauss' divergence theorem, green's theorem, and stokes' theorem.
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(^) b a f^ (x)^ dx. Here^ a^ and^ b^ could involve other variables besides^ x. Use Calculus I and II to solve these.
C M dx^ +^ N dy^ +^ P dz^ or^
C f ds. Use this three-step procedure: (a) Parametrize C in terms of t, say, with a ≤ t ≤ b. (b) Compute dierentials dx, dy, dz, ds as needed. (c) Reduce line integral to a denite integral on interval a ≤ t ≤ b by substitution.
(^) b a
(^) g(v) f (v) F^ (u, v)^ du dv^ or^
(^) b a
(^) g(w) f (w)
(^) h(v,w) g(v,w) F^ (u, v, w)^ du dv dw.^ These are just denite integrals two or three times.
R f dA^ or^
D f dV^. Use a Fubini-type theorem to reduce these to iterated integrals.
S f dσ. Use this three-step procedure: (a) Parametrize S in terms of u, v, say, with (u, v) ∈ R, a region in the uv-plane and write out a position vector r (u, v) = 〈x (u, v) , y (u, v) , z (u, v)〉 for points on S. (b) Compute dierential dσ = |ru × rv| dA, where dA is dierential area in uv-plane. Important special case where this is precomputed:√ If S is the graph of z = f (x, y), then dσ = f (^) x^2 + f (^) y^2 + 1 dA, where dA is dierential area in the xy-plane. (c) Reduce surface integral to a double integral over R by substitution.
S F^ ·^ n^ dσ. Here^ n^ is a continuous unit normal vector to^ S. Use same three-step procedure as in 5, except that in (b) n dσ = ±ru × rv dA. Important special case where this is precomputed: If S is the graph of z = f (x, y), then n dσ = ± 〈−fx, −fy, 1 〉 dA, where dA is dierential area in the xy-plane.
The idea is to indirectly calculate one side by directly calculating the other side of one of the following theorems.
S
F · n dσ =
D
∇ · F dV
Here the boundary of the solid D is the (closed) surface S = ∂D with outward pointing normal n.
C
F · n ds = C
M dy − N dx =
R
(Mx + Ny) dA =
R
∇ · F dA
C
F · dr =
S
∇ × F · n dσ
Here C = ∂S is the closed boundary of the surface S, positively oriented with respect to the surface normal n.
C
F · dr = C
M dx + N dy =
R
(Nx − My) dA =
R
∇ × F · k dA