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112 Angermann and Yatsyk<br />

+ 1 4<br />

∑<br />

χ (3)<br />

⎧<br />

n,m,p∈Z\{0}<br />

⎪⎨ n≠−m, p=s<br />

m≠−p, n=s<br />

⎪⎩ n≠−p, m=s<br />

n+m+p=s<br />

1111 (sω; nω, mω, pω)E 1(r, nω)E 1 (r, mω)E 1 (r, pω), (5)<br />

·<br />

where the symbol = means that higher-order terms are neglected.<br />

If we study nonlinear effects involving the waves at the first<br />

three frequency components of E 1 only, it is possible to restrict the<br />

system (4), (5) to three equations. Then the analysis of the scattering<br />

problem for the plane wave packet<br />

{<br />

E1 inc (r, nκ) := E1 inc (nκ; y, z) := a inc<br />

nκ exp<br />

(i ( φ nκ y − Γ nκ (z − 2πδ) ))} 3<br />

, (6)<br />

z > 2πδ, δ > 0, with amplitudes a inc<br />

nκ, angles of incidence ϕ nκ ,<br />

|ϕ| < π/2<br />

√<br />

(cf. Figure 1) and κ := ω/c = 2π/λ, φ nκ := nκ sin ϕ nκ ,<br />

Γ nκ := (nκ) 2 − φ 2 nκ, on the nonlinear structure can be simplified by<br />

means of Kleinman’s rule (i.e., the equality of all the coefficients χ (3)<br />

1111<br />

at the multiple frequencies, [10, 12]) and reduces finally to the following<br />

system of boundary-value problems ([4–6, 11, 17]):<br />

[<br />

∇ 2 +κ 2 ε κ (z, α(z), E 1 (r, κ), E 1 (r, 2κ), E 1 (r, 3κ)) ] × E 1 (r, κ)<br />

= −α(z)κ 2 E 2 1(r, 2κ)Ē1(r, 3κ),<br />

[<br />

∇ 2 +(2κ) 2 ε 2κ (z, α(z),E 1 (r, κ),E 1 (r, 2κ),E 1 (r,3κ)) ] ×E 1 (r, 2κ)=0,<br />

[<br />

∇ 2 +(3κ) 2 ε 3κ (z, α(z), E 1 (r, κ), E 1 (r, 2κ), E 1 (r, 3κ)) ] × E 1 (r, 3κ)<br />

= −α(z)(3κ) 2{ 1<br />

}<br />

3 E3 1(r, κ) + E1(r, 2 2κ)Ē1(r, κ) ,<br />

where κ := ω/c = 2π/λ,<br />

{<br />

ε nκ := ε (L) + ε (NL)<br />

nκ , |z| ≤ 2πδ,<br />

and ε (L) := 1 + 4πχ (1)<br />

11<br />

1, |z| > 2πδ,<br />

,<br />

[<br />

ε (NL)<br />

nκ<br />

:= α(z)<br />

|E 1 (r, κ)| 2 + |E 1 (r, 2κ)| 2 + |E 1 (r, 3κ)| 2<br />

[Ē1 (r, κ) ] ]<br />

2<br />

+δ n1<br />

E 1 (r, κ) E Ē 1 (r, 2κ)<br />

1(r, 3κ)+δ n2<br />

E 1 (r, 2κ) E 1(r, κ)E 1 (r, 3κ)<br />

with α(z) := 3πχ (3)<br />

1111 (z) and δ nm — Kronecker’s symbol. In addition,<br />

the following conditions are met (n = 1, 2, 3):<br />

(C1) E 1 (nκ; y, z) = U(nκ; z) exp(iφ nκ y),<br />

(the quasi-homogeneity condition w.r.t. y),<br />

n=1<br />

(7)

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