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(1)

We will prove that the improper integral Γ(x) =

Z 0

e−ttx−1dt

exists for every x > 0. The function Γ(x) is called the Gamma function. Let us recall the comparison test for improper integrals.

Theorem 1.1. (Comparison Test for Improper Integral of Type I) Let f (x), g(x) be two continuous functions on [a, ∞) such that 0 ≤ f (x) ≤ g(x) for all x ≥ a. Then

(1) If Z

a

g(x)dx is convergent, so is Z

a

f (x)dx.

(2) If Z

a

f (x)dx is divergent to infinity, so is Z

a

g(x)dx.

Theorem 1.2. (Limit Comparison Test) Let f (x), g(x) be two nonnegative continuous functions on [a, ∞). Suppose that

x→∞lim f (x)

g(x) = L with L > 0.

Then both Z

a

g(x)dx and Z

a

f (x)dx are convergent or divergent.

Lemma 1.1. For every s > 0, the improper integral Z

0

e−stdt converges.

Proof. Let us compute

Z N 0

e−stdt = e−sM− 1

−s . By definition,

Z 0

e−stdt = lim

N →∞

Z N 0

e−stdt = lim

N →∞

e−sM − 1

−s = 1

s.

The limit exists and hence the improper integral converges.  Now let us study the case when x ≥ 1.

Lemma 1.2. Let n be a natural number. Then

t→∞lim tn−1

e12t = 0.

Proof. By L’ Hospital rule,

t→∞lim tn−1

e12t

= lim

t→∞

(n − 1)tn−2

1 2e12t

. Since tn−1 is a polynomial of degree n − 1, we know

dn

dtntn−1= 0.

Inducitvely, we find

t→∞lim tn−1

e12t = lim

t→∞

0

1 2

n

e12t = 0.



1

(2)

By the definition of limit, we choose  = 1, there exists M > 0 such that for all t ≥ M

tn−1 e12t

<  = 1.

Hence for t ≥ M, 0 ≤ tn−1< e12t. This implies that for t ≥ M, (1.1) 0 ≤ e−ttn−1≤ e−t· e12t= e12t. Lemma 1.1 implies that

Z 0

e12tdt is convergent. (1.1) and Comparison test implies that Z

0

e−ttn−1dt is convergent for every n ∈ N.

Let x ≥ 1 be any real number. Let [x] be the largest integer so that [x] ≤ x < [x] + 1.

Then for t ≥ 0,

(1.2) 0 ≤ e−ttx−1 ≤ e−tt[x].

Since Z

0

e−tt[x]dx is convergent, by comparison test and (1.2), we find Z

0

e−ttx−1dt is convergent.

Now let us study the case when 0 < x < 1. Then we know 1

e12t

≤ tx−1 e12t

≤ t e12t. We know that

t→∞lim t

e12t = lim

t→∞

1 e12t = 0.

By the Sandwich principle,

t→∞lim tx−1

e12t

= 0

for 0 < x < 1. (Of course, this statement is true for all x > 0.) This implies that 0 ≤ e−ttx−1 ≤ e12t, t ≥ 1.

By comparison test, Z

1

e−ttx−1dt is convergent for 0 < x < 1. Now, we need to verify that Z 1

0

e−ttx−1dt = Z 1

0

et t1−xdt is convergent. Notice that lim

t→0

e−t

t1−x = ∞. Hence the integral Z 1

0

e−ttx−1dt is a type II improper integral.

Theorem 1.3. Let f, g ∈ C(a, b] and 0 ≤ f (x) ≤ g(x) for all a < x ≤ b.

(1) If Z b

a

g(x)dx is convergent, so is Z b

a

f (x)dx.

(2) If Z b

a

f (x)dx is divergent to infinity, so is Z b

a

g(x)dx.

(3)

Note that

0 < e−ttx−1 ≤ etx−1. We know that

Z 1 0

tx−1dt = lim

b→0

Z 1 b

tx−1dt

= lim

b→0

tx x

1

b

= lim

b→0

 1 x −bx

x



= 1 x. By the comparison test,

Z 1 0

e−ttx−1dt is convergent.

Theorem 1.4. For every x > 0, the improper integral Γ(x) =

Z 0

e−ttx−1dt is convergent.

Proposition 1.1. For x > 0,

Γ(x + 1) = xΓ(x).

Proof. For every N > 0, using integration by parts, Z N

0

e−ttxdt = −txe−t

N 0 + x

Z N 0

e−ttx−1dt

= −Nxe−N + x Z N

0

e−ttx−1dt.

We have seen that lim

N →∞Nxe−N = lim

N →∞

Nx

eN = 0 for all x > 0. Then Γ(x + 1) = lim

N →∞

Z N

0

e−ttxdt

= lim

N →∞(−Nxe−N+ x Z N

0

e−ttx−1dt)

= x lim

N →∞

Z N 0

e−ttx−1dt

= xΓ(x).

 Corollary 1.1. For every n ≥ 0, Γ(n + 1) = n!.

Proof. We know Z

0

e−tdt = 1. Hence Γ(1) = 1. We can prove the formula by induction.

Assume that the statement is true for some nonnegative integer k, i.e. Γ(k + 1) = k!. By the previous proposition,

Γ(k + 2) = Γ((k + 1) + 1) = (k + 1)Γ(k + 1) = (k + 1) · k! = (k + 1)!.



(4)

Proposition 1.2. For any s > 0, x > 0, we have Z

0

e−sttx−1dt = Γ(x) sx .

Proof. This formula can be proved by using substitution u = st.

 Example 1.1.

Z 0

e−st(2 − 3t + 5t2)dt = 2 s− 3

s2 +10 s3. This can be proved by the previous proposition.

Here comes a question, if f (t) is a continuous function on [0, ∞) such that Z

0

e−stf (t)dt = 2 s− 3

s2 + 10 s3,

what can you say about f (t)? Let us introduction the notion of Laplace transformation.

(5)

2. Laplace Transformation, its inverse transformation, and linear homogeneous o.d.e of constant coefficients

Definition 2.1. Let f (t) be a continuous function on [0, ∞). Suppose Z

0

e−stf (t)dt con- verges for s ≥ a for some a ∈ R. Denote

L(f )(s) = Z

0

e−stf (t)dt called the Laplace transform of f.

Now, let us assume that the Laplace transform of f1, f2 exist on some domain D ⊂ R where f1, f2 are continuous functions on [0, ∞). For any real numbers a1, a2, we know that for any s ∈ D,

L(a1f1+ a2f2)(s) = Z

0

(a1f1(t) + a2f2(t))e−stdt

= lim

M →∞

Z M 0

(a1f1(t) + a2f2(t))e−stdt

= lim

M →∞

 a1

Z M 0

f1(t)e−stdt + a2 Z M

0

f2(t)e−stdt



= a1 lim

M →∞

Z M 0

f1(t)e−stdt + a2 lim

M →∞

Z M 0

f2(t)e−stdt

= a1L(f1)(s) + a2L(f2)(s).

Proposition 2.1. Suppose that f1, f2 are two continuous functions on [0, ∞) such that their Laplace transform exist on some domain D ⊂ R for s. Then

L(a1f1+ a2f2)(s) = a1L(f1)(s) + a2L(f2)(s), s ∈ D,

for any a1, a2∈ R. (We say that the Laplace transform is a linear transformation.)

Theorem 2.1. Suppose f1, f2 are two continuous functions on [0, ∞) such that their Laplace transform exist. If L(f1) = L(f2), then f1 = f2.

Hence if g(s) = L(f )(s), we denote

f (t) = L−1(g)(t) called then Laplace inverse transform.

Proposition 2.2. Suppose f (t) is a smooth function on [0, ∞) (f(k)(t) exists for all k ≥ 1.

Set f(0)(t) = f (t).) Assume that lim

t→∞f(k)(t)e−st= 0 for all k ≥ 0. Then L(f0)(s) = −f (0) + sL(f )(s).

Proof. Using integration by parts, Z N

0

e−stf0(t)dt = f (t)e−st

N 0 + s

Z N 0

e−stf (t)dt

= f (N )e−sN− f (0) + s Z N

0

e−stf (t)dt.

(6)

By assumption, lim

N →∞f (N )e−sN = 0 (consider k = 0.) Hence Z

0

e−stf0(t)dt = lim

N →∞

Z N 0

e−stf0(t)dt

= lim

N →∞



f (N )e−sN − f (0) + s Z N

0

e−stf (t)dt



= −f (0) + s lim

N →∞

Z N 0

e−stf (t)dt

= −f (0) + s Z

0

e−stf (t)dt.

 Corollary 2.1. Under the same assumption as above, we have

L(f(n))(s) = snF (s) −X

k=0

sn−k−1f(k). When n = 2, we have L(f00)(s) = s2F (s) − sf0(0) − f (0).

Now let us use Laplace transform to solve ordinary differential equation with constant coefficients.

Example 2.1. Solve for y0+ 2y = 0 with initial condition y(0) = 1.

Take Laplace transform, we obtain

L(y0+ 2y)(s) = L(y0)(s) + 2L(y)(s) = 0.

Let g(s) = L(y)(s). Using the previous proposition,

L(y0)(s) = −y(0) + sL(y)(s) = −1 + sg(s).

Hence (−1 + sg(s)) + 2g(s) = 0. This implies that g(s) = 1

s + 2. Then y = L−1(g)(t) = e−2t.

Example 2.2. Solve for y00+ y = 0 with initial condition y(0) = a and y0(0) = b.

Let g(s) be the Laplace transform of y. Then

L(y00)(s) + g(s) = 0.

On the other hand, L(y00)(s) = s2g(s) − sy(0) − y0(0) = s2g(s) − as − b. This implies that (s2+ 1)g(s) = as + b =⇒ g(s) = a s

s2+ 1+ b 1 s2. We know s

s2+ 1 = L(cos t)(s), and 1

s2+ 1 = L(sin t)(s). Hence y(t) = a cos t + b sin t.

In general, we can solve for the linear (homogeneous) differential equation of constant coefficients through Laplace transformation. A linear homogeneous differential equation of constant coefficients is a differential equation

(2.1) any(n)+ an−1y(n−1)+ · · · + a1y0+ a0y = 0, where a0, · · · , an∈ R. If an6= 0, we say that the equation is of order n.

Let us study the case when n = 2 :

(2.2) ay00+ by0+ cy = 0.

(7)

Here a 6= 0. Taking the Laplace transformation of the equation, we have a(s2F (s) − sy0(0) − y(0)) + b(sF (s) − y(0)) + cF (s), where F (s) = L(y)(s). Therefore F (s) is a rational function in s and given by

F (s) = As + B as2+ bs + c.

where A = ay0(0) and B = ay0(0) + by(0). We can use partial fraction expansion to decom- pose F (s).

Definition 2.2. The polynomial χ(s) = as2+ bs + c is called the characteristic polynomial of (2.2).

We assume that a = 1 and let D = b2 − 4c be the discriminant of the characteristic polynomial.

case 1: If D > 0, χ(s) has two distinct real roots. We denote the root of χ(s) by λ1 and λ2. Thus we may write

F (s) = C1

1 s − λ1

+ C2

1 s − λ2

for some C1, C2∈ R. We know that

L(eat)(s) = 1 s − a.

Using the inverse transform and the linearity of L−1, we see that y(t) = L−1(F )(t)

= C1L−1

 1

s − λ1



+ C2L−1

 1

s − λ2



= C1eλ1t+ C2eλ2t. Hence y is a linear combination of eλ1t and eλ2t.

case 2: If D = 0, χ(s) has one repeated root, called λ. Then we write F (s) = C1

1

s − λ + C2

1 (s − λ)2. Recall that

L(tneλt)(s) = Z

0

e−sttnedt = Γ(n + 1)

(s − λ)n+1 = n!

(s − λ)n+1. Thus we obtain

y(t) = L−1(F )(t)

= C1L−1

 1 s − λ



+ C2L−1

 1

(s − λ)2



= C1eλt+ C2teλt

= (C1+ C2t)eλt.

case 3: If D < 0, by completing the square, we write χ(s) = (s − α)2+ β2. We write

F (s) = As

(s − α)2+ β2 + B

(s − α)2+ β2 = C1 s − α

(s − α)2+ β2 + C2 β

(s − α)2+ β2.

(8)

Notice that

L(eαtcos βt)(s) = s − α

(s − α)2+ β2, L(eαtsin βt) = β

(s − α)2+ β2. Thus

y(t) = L−1(F )(t)

= C1L−1

 s − α (s − α)2+ β2



+ C2L−1

 β

(s − α)2+ β2



= C1eαtcos βt + C2eαtsin βt

= eαt(C1cos βt + C2sin βt).

Remark. Let V be the subset of C2[0, ∞) consisting of y such that (2.2) holds. The above observation implies that V is in fact a two dimensional real vector (sub)space (of C2[0, ∞)).

This method can be applied to (2.1) for any n ∈ N.

Definition 2.3. The characteristic polynomial of (2.1) is defined to be χ(s) = ansn+ · · · + a1s + a0.

Taking the Laplace transformation of (2.1) and using Corollary 2.1, we find that F (s) = P (s)

χ(s)

for some polynomial P (s) ∈ R[s]. Thus F (s) is a rational function and we can solve for y using the partial fraction for F (s). Thus we reduce our problems to the cases when χ(s) = (s − a)nor χ(s) = ((s − α)2+ β2)m. When χ(s) = (s − a)n, we write

F (s) = A1

s − a + A2

(s − a)2 + · · · + An (s − a)n

= C0 1

s − a + C1 1!

(s − a)2 + · · · + Cn−1(n − 1)!

(s − a)n,

where Ci−1= Ai/(i − 1)! for i = 1, · · · , n. By taking the inverse transform, we obtain y(t) = (C0+ C1t + · · · + Cn−1tn−1)eat.

When χ(s) = ((x − α)2+ β2)m, we write F (s) = A1s + B1

(x − α)2+ β2 + · · · + Ams + Bm

((s − α)2+ β2)m

= C1(s − a) + D1β

(x − α)2+ β2 + · · · + Cm(s − a) + Dmβ ((s − α)2+ β2)m .

Here Ci, Dj are constants. By finding the inverse transform of (Ci(s − a) + Diβ)/(((s − α)2+ β2)i), we obtain y.

(9)

3. Beta Function In this section, x, y are positive real numbers. Let us define

B(x, y) = Γ(x)Γ(y) Γ(x + y).

The function B(x, y) is called the Gamma function. It follows immediately from the defi- nition that

B(x, y) = B(y, x), ∀x, y > 0.

Using the property of Gamma function: Γ(x + 1) = xΓ(x) for x > 0, we obtain:

Proposition 3.1. Suppose p, q > 0. Then (1) B(p, q) = B(p + 1, q) + B(p, q + 1).

(2) B(p, q + 1) = q

pB(p + 1, q) = q

p + qB(p, q).

Theorem 3.1. For x, y > 0,

B(x, y) = Z

0

tx−1 (1 + t)x+ydt.

Let us postpone the proof of this equation.

Let us consider the substitution t = tan2θ with 0 ≤ θ ≤ π/2. Then dt = 2 tan θ sec2θdθ.

Using sec2θ = tan2θ + 1, Beta function B(x, y) can be rewritten as B(x, y) =

Z π

2

0

(tan2θ)x−1

(1 + tan2θ)x+y · 2 tan θ sec2θdθ

= 2 Z π

2

0

tan2x−2θ

sec2x+2yθ · tan θ sec2θdθ

= 2 Z π

2

0

tan2x−1θ · 1

sec2x+2y−2θdθ

= 2 Z π

2

0

 sin θ cos θ

2x−1

· cos2x+2y−2θdθ

= 2 Z π

2

0

sin2x−1θ cos2y−1θdθ.

Using B(y, x) = B(x, y), we also obtain B(x, y) = 2

Z π

2

0

cos2x−1θ sin2y−1θdθ.

This is the second form of Beta function. Consider substitution t = sin2θ for 0 ≤ θ ≤ π/2.

Then dt = 2 sin θ cos θdθ, we obtain the third form of the Beta function:

B(x, y) = Z 1

0

tx−1(1 − t)y−1dt.

We conclude that

Theorem 3.2. The Beta function has the following forms:

(1) B(x, y) = Z

0

tx−1 (1 + t)x+ydt,

(10)

(2) B(x, y) = 2 Z π2

0

cos2x−1θ sin2y−1θdθ, (3) B(x, y) =

Z 1 0

tx−1(1 − t)y−1dt.

Example 3.1. Compute Z

0

e−x2dx.

Let us make a change of variable t = x2. Then dt = 2xdx and thus dx = t12dt 2 .The integral can be rewritten as

Z 0

e−x2dx = 1 2

Z 0

e−tt12dt = Γ 12 2 . Now, we only need to compute Γ(1/2). Using Beta function,

B 1 2,1

2



= Γ 122

Γ 12 +12 = Γ

 1 2

2

On the other hand, B 1

2,1 2



= 2 Z π

2

0

cos12−1θ sin12−1θdθ = 2 Z π

2

0

dθ = π.

Hence Γ(1/2) =√

π. We obtain that Z

0

e−x2dx =

√π 2 . Example 3.2. Compute

Z 0

sin4θdθ.

We know Z

0

sin4θdθ = 4 Z π

2

0

sin4θdθ = 2 · 2 Z π

2

0

sin52−1θ cos12 θdθ = 2B 5 2,1

2

 . We compute

B 5 2,1

2



= Γ 52 Γ 12 Γ(3) . Using Γ(x + 1) = xΓ(x), we obtain

Γ 5 2



= 3 2 ·1

2· Γ 1 2



= 3 4

√π.

Hence B 5 2,1

2



=

3 4

√π ·√ π

2! = 3

8π. Thus Z

0

sin4θdθ = 3 4π.

Now, let us go back to the proof of Theorem 3.1.

Γ(x)Γ(y) =

Z 0

e−ttx−1dt

 Z 0

e−ssx−1ds



= Z

0

Z 0

e−(t+s)tx−1sy−1dtds.

(11)

Let us compute Z

0

e−(t+s)tx−1dt. Consider t = su, we rewrite Z

0

e−(t+s)tx−1dt = sx Z

0

e−(u+1)sux−1du.

Hence the integral becomes Γ(x)Γ(y) =

Z 0

Z 0

e−(u+1)ssx+y−1ds



ux−1du

= Z

0

Γ(x + y)

(u + 1)x+y · ux−1du

= Γ(x + y) Z

0

ux−1 (1 + u)x+ydu.

Here we use Proposition 1.2. This shows that Γ(x)Γ(y)

Γ(x + y) = Z

0

ux−1 (1 + u)x+ydu.

Example 3.3. Compute Z 3

1

(x − 1)10(x − 3)3dx.

Let t = (x − 1)/2. Then the integral becomes Z 3

1

(x − 1)10(x − 3)3dx = Z 1

0

(2t)10(2t − 2)32dt = −214 Z 1

0

t10(1 − t)3dt.

We obtain

Z 3 1

(x − 1)10(x − 3)3dx = −214B(11, 4) = −214·10!3!

14! .

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