• No results found

A boundary layer of thickness O ( √ ε)

N/A
N/A
Protected

Academic year: 2022

Share "A boundary layer of thickness O ( √ ε)"

Copied!
29
0
0

Laster.... (Se fulltekst nå)

Fulltekst

(1)

Principal of least degeneracy

Higher order matching and nonlinear equations

Lesson 16

(2)

A boundary layer of thickness O ( √ ε)

Let us consider the example εddx2f2 + x2dxdf f = 0 with

x (0, 1), f(0) = 1, f(1) = 2. We will look for the one

term expansion. Since x2 > 1 on (0, 1) we assume that the boundary layer is at x = 0. Is something strange up to now? Thus

x2df0out

dx f0out = 0, f0out(1) = 2.

Separating variables leads to

Z df0out f0out =

Z dx

x2 f0out = Ce1/x = 2e11/x.

(3)

Thickness O( √ ε)

We suppose that s = x/ε, then the new equation is

d2f

ds2 + ε2s2 df

ds εf = 0, f(0) = 1

then

d2f0in

ds2 = 0 f0in = As + 1.

Applying matching condition, we get

xlim0 2e11/x = lim

s→∞

As + 1.

What is wrong?

(4)

Thickness O( √ ε)

Let us try the stretched variable s = x/εp, then

df

dx = 1 εp

df

ds, d2f

dx2 = 1 ε2p

d2f ds2 . ε12p d2f

ds2 + εps2 df

ds f = 0.

Let us try to keep the maximum number of terms in the equation. Taking p = 1/2 we keep the second derivative and f. Then

d2f0in

ds2 f0in = 0, f0in(0) = 1, f0in = Aes + (1 A)es.

(5)

Thickness O( √ ε)

Applying Prandtl’s matching condition, we get

xlim0 2e11/x = lim

s→∞

Aes + (1 A)es

that implies A = 2. Thus

f0comp = 2e11/x + ex/ε.

If p < 1/2 then f0in = 0 which does not satisfy the boundary condition at s = 0.

(6)

An interior boundary layer

εd2f

dx2 +xdf

dx+xf = 0 with x (1, 1), f(1) = e, f(1) = 2e1. We expect the boundary layer at x = 0, two outer

solution f0+out = f0+ and f0out = f0. We have

df0+

dx + f0+ = 0, f0+(1) = 2e1 f0+ = 2ex, df0

dx + f0 = 0, f0(1) = e f0 = ex.

(7)

An interior boundary layer

The stretched variable s = x/εp leads to

ε12p d2f

ds2 + sdf

ds + εpsf = 0.

Taking p = 1/2, we get

d2f0in

ds2 + sdf0in

ds = 0.

We make a substitution w = dfds0in, then

dw + sw = 0 w = Aes2/2

(8)

An interior boundary layer

f0in = A

Z s

0

et2/2 dt + f0in(0).

We write R0s et2/2 dt = 12 R0s/2 eu2 du = B erf(s/2). Then

f0in = B erf(s/

2) + f0in(0).

The Prandtl’s condition gives

xlim0+ 2ex = lim

s+

B erf(s/

2) +f0in(0) B+f0in(0) = 2,

xlim0 ex = lim

s+

B erf(s/

2)+f0in(0) ⇒ −B+f0in(0) = 1.

(9)

An interior boundary layer

B = 1/2, f0in(0) = 3/2.

Summarizing

f0+ = 2ex, x > O( ε) f0in = 1/2 erf(x/

2ε) + 3/2, x = O( ε) f0 = ex, x < O(

ε)

The composition solution can not be produced by the standard way. We observe

(10)

An interior boundary layer

f0in

x > O(

ε)

= 1/2 + 3/2 + sm. t., since erf 1,

f0in

x < O(

ε)

= 1/2 + 3/2 +sm. t., since erf ∼ −1, We conclude that

f0comp =

1/2 erf(x/

2ε) + 3/2

ex.

(11)

An interior boundary layer

(12)

Higher order matching

We shall work with the old example

εd2f

dx2 + df

dx = 2x + 1, x (0, 1), f(0) = 1, f(1) = 4, fex = x2 + x + 2 ex/ε + ε

2(1 x) 2ex/ε

Using the stretched variable s = x/ε we get

(13)

Higher order matching

d2f

ds2 + df

ds = 2ε2s + ε, f(s, ε) f0(s) + εf1(s) + . . . , ε0 d2f0in

ds2 + df0in

ds = 0, f0in(0) = 1 f0in = A + (1 A)es ε1 d2f1in

ds2 + df1in

ds = 1, f1in(0) = 0 f1in = B Bes + s ε2 d2f2in

ds2 + df2in

ds = 2s, f2in(0) = 0 f2in = C Ces + s2 2s εn d2fnin

ds2 + dfnin

ds = 0, fnin(0) = 0 fnin = Dn Dnes,

(14)

Higher order matching

fin = A + (1 A)es + ε(B Bes + s) 2(C Ces + s2 2s) +

X

n=3

εnDn(1 es).

The Prandtl’s condition can not be applied, because of existence of unbounded terms εs and ε2(s2 2s). They represent x and x2 2εx. Let us write the exact

solution in terms of s:

(15)

Higher order matching

fex = x2 + x + 2 ex/ε + ε

2(1 x) 2ex/ε

= ε2s2 + εs + 2 es + ε 2(1 εs) 2es

= 2 es + ε(2 2es + s) + ε2(s2 2s).

Comparing with fin we get A = 2, B = 2, C = 0, Dn = 0,

n = 3, 4, . . .. How we can define A, B, C, Dn without of exact solution?

(16)

Higher order matching

Let us look on the Prandtl’s condition from the other point of view. Let x = O(ε1/2), then

fin = A+(1A)es = A+o(1), fout = x2+x+2ex/ε = 2+o(1).

We recuperated A = 2. Let us do the same, but in slightly general form. We represent s = xε in two

variables x = α then s = ε1tα . Let us represent two term expansion in terms of new variable t = x/εα,

α (0, 1) for t fixed. We get

fout = x2 + x + 2 + ε2(1 x) = 2 + εαt + εt2 + 2ε 1+αt

(17)

Higher order matching

Now we use s = ε1tα and fined two term expansion of

fin in terms of ε1tα .

fin = A + ε(B + s) = A + εαt + εB.

Matching with

fout = 2 + εαt + εt2 + 2ε 1+αt

we have to ask ε = o(ε), or α > 1/2. We get A = 2 and

B = 2.

(18)

Higher order matching

The composition solutions is

f2compterm = f2outterm + f2interm f2matchterm

where f2compterm is given by terms of order up to O(ε). In our case it is 2 + x + 2ε. We have

fcomp = x2 + x + 2 + 2ε(1 x) +2 ex/ε + ε(2 2ex/ε + x/ε)

2 x = x2 + x + 2 ex/ε + ε(2 2x 2ex/ε).

(19)

Nonlinear examples

εd2f

dx2 + df

dx + f2 = 0, x (0, 1), f(0) = 2, f(1) = 1/2.

df0out

dx + (f0out)2 = 0, f0out(1) = 1/2 f0out = 1 x + 1. s = x

ε d2fin

ds2 + dfin

ds + ε(fin)2 = 0 d2f0in

ds2 + df0in

ds = 0 f0in = A + (2 A)es

(20)

Nonlinear examples

The Prandtl’s condition implies

xlim0

1

x + 1 = lim

s→∞

A + (2 A)es A = 1.

fcomp = 1

x + 1 + ex/ε.

(21)

Nonlinear examples

εd2f

dx2 + 2f df

dx 4f = 0, x (0, 1), f(0) = 0, f(1) = 4.

2f0outdf0out

dx 4f0out = 0, f(1) = 4 f0out = 2x + 2 s = x

ε d2f0in

ds2 +2f0indf0in

ds = 0 d ds

df0in

ds +(f0in)2

= 0 df0in

ds + (f0in)2 = c = a2

since f0in(0) = 0 and lim

x 0 f0out = 2 and f0in increase

(22)

Nonlinear examples

R df0in

a2(f0in)2 = R

ds

2a1 R df0in

f0ina + 2a1 R df0in

f0in+a = s + b

ln |f0in a| + ln |f0in + a| = 2as + 2ab

f0ina

f0in+a = Ae2as, A = ±e2ab

A = 1, f0in = aee22asas+11 = a tanh as

lim

x0 f0out = lim

s→∞

f0in a = 2

(23)

Nonlinear examples

R df0in

a2(f0in)2 = R

ds

2a1 R df0in

f0ina + 2a1 R df0in

f0in+a = s + b

ln |f0in a| + ln |f0in + a| = 2as + 2ab

f0ina

f0in+a = Ae2as, A = ±e2ab

A = 1, f0in = aee22asas+11 = a tanh as

lim

x0 f0out = lim

s→∞

f0in a = 2

(24)

Nonlinear examples

R df0in

a2(f0in)2 = R

ds

2a1 R df0in

f0ina + 2a1 R df0in

f0in+a = s + b

ln |f0in a| + ln |f0in + a| = 2as + 2ab

f0ina

f0in+a = Ae2as, A = ±e2ab

A = 1, f0in = aee22asas+11 = a tanh as

lim

x0 f0out = lim

s→∞

f0in a = 2

(25)

Nonlinear examples

R df0in

a2(f0in)2 = R

ds

2a1 R df0in

f0ina + 2a1 R df0in

f0in+a = s + b

ln |f0in a| + ln |f0in + a| = 2as + 2ab

f0ina

f0in+a = Ae2as, A = ±e2ab

A = 1, f0in = aee22asas+11 = a tanh as

lim

x0 f0out = lim

s→∞

f0in a = 2

(26)

Nonlinear examples

R df0in

a2(f0in)2 = R

ds

2a1 R df0in

f0ina + 2a1 R df0in

f0in+a = s + b

ln |f0in a| + ln |f0in + a| = 2as + 2ab

f0ina

f0in+a = Ae2as, A = ±e2ab

A = 1, f0in = aee22asas+11 = a tanh as

lim

x0 f0out = lim

s→∞

f0in a = 2

(27)

Nonlinear examples

R df0in

a2(f0in)2 = R

ds

2a1 R df0in

f0ina + 2a1 R df0in

f0in+a = s + b

ln |f0in a| + ln |f0in + a| = 2as + 2ab

f0ina

f0in+a = Ae2as, A = ±e2ab

A = 1, f0in = aee22asas+11 = a tanh as

lim

x0 f0out = lim

s→∞

f0in a = 2

(28)

Nonlinear examples

f0in = a tanh 2s

fcomp = 2x + 2 tanh(2x/ε).

(29)

The end

Referanser

RELATERTE DOKUMENTER

When assuming a second order concentration profile the boundary layer thickness can easily be calculated from the total mass and the concentration pro- file.. For the error

In order to study the effect of the spackling layer thickness, supply air temperatures, and the air flow rate on the performance of the spackling PCM, a parametric analysis

These results and calculations shows that (a) increasing the air velocity decreases the boundary layer thickness, hence leading to a higher convective moisture transfer

The influence of halogen oxidation on the variabil- ities of ozone (O 3 ) and volatile organic compounds (VOCs) within the Arctic and sub-Arctic atmospheric boundary layer

Representative spectra of N ε - and O-acetylated peptides in Mtb (Figure S1); protein − protein interaction network analysis of N ε - and O-acetylated proteins in Mtb (Figure S2);

Chapter 9: present the results from the numerical solution to the non-dimensionalized boundary layer problem and compare the boundary layer obtained from the NSS system with

This report presents LES results using a synthetic turbulence generator to supply artificial inflow conditions for two high Reynolds number turbulent boundary layer flows.. In

Also a few other cases (see table 4.1) shows.. This supports the hypothesis that the mean stream wise velocity in the linear sub-layer is the appropriate velocity scale for