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Молодой учёный

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6 Математика<br />

«<strong>Молодой</strong> <strong>учёный</strong>» . № 3 (50) . Март, 2013 г.<br />

Fig. 1. Trajectories<br />

These characteristics defi ne two trajectories for t∈ [ tk-1, tk]<br />

in plane ( t, x ): C (t, x (t)), i =1,2. Each of these trajectories<br />

i i<br />

crosses line t = t in some point ( t k -1<br />

k- 1,<br />

Ai).<br />

We suppose that they are not mutually crossed and therefore 1 2 . A A <<br />

Theorem 1. For smooth solution of equation (1) we have equality<br />

x2 A2<br />

∫ ∫<br />

r( t , x) dx = r( t - , x) dx.<br />

x<br />

k k 1<br />

1 A1<br />

Proof. Defi ne by G the curvilinear quadrangle bounded by lines t = tk, C2, t = tk-1, C1.<br />

And defi ne by Γ1, Γ2, Γ3, Γ 4<br />

the corresponding parts of these lines, which form the boundary Γ = Γ1∪Γ2 ∪Γ3 ∪Γ (see Fig. 2). Introduce also the ex-<br />

4<br />

ternal normal n defi ned at each part of boundary except 4 vertices of quadrangle.<br />

Now use formula by Gauss-Ostrogradskii [16, 17] in the following form:<br />

G<br />

⎛∂r ∂(<br />

ru)<br />

⎞<br />

<br />

⎜ + ⎟ dG = ( rr , u) ⋅ndΓ ⎝ ∂t ∂x<br />

⎠<br />

∫ ∫<br />

Γ<br />

where sing ⋅ means scalar product. Since the boundary Γ consists of four parts we calculate the integral over Γ separately<br />

on each line:<br />

<br />

( rr , u) ⋅ndΓ= ( rr , u) ⋅ndΓ+ ( rr , u) ⋅ndΓ+ ( rr , u) ⋅ndΓ+ ( rr , u) ⋅ndΓ. ∫ ∫ ∫ ∫ ∫<br />

Γ Γ1 Γ2 Γ3 Γ4<br />

Fig. 2. Integration along boundary<br />

Along the line 1 Γ the external normal equals n = (1,0). Then<br />

<br />

x2<br />

∫( rr , u) ⋅ndΓ=-∫ r(<br />

tk , x) dx.<br />

x1<br />

Γ1<br />

Minus appeared in right-hand side because of opposite direction of integration. At arbitrary point (, tx) ∈ C2the<br />

tangent<br />

vector is v(t, x) = (1, u(t, x)). Therefore the external normal equals<br />

<br />

n =<br />

1<br />

u 2 +1<br />

Therefore we get<br />

(u, –1). -1).<br />

<br />

dΓ<br />

( rr , u) ⋅ndΓ= ( rr , u) ⋅( u,<br />

- 1) = 0.<br />

2<br />

u + 1<br />

∫ ∫<br />

Γ2 Γ2<br />

(4)<br />

(5)<br />

(6)<br />

(7)<br />

(8)<br />

(9)

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