6.3 Proof of flux theoremThis section of the tutorial contains the proof of the flux theorem listed in the previous page. The proof is broken into intermediate results which are listed in theorems, lemmas, etc., which lead to the proof of the flux theorem. Since this page is a little more dense than the others, one can skip this page on a first reading and come back to it later. Since our flow is Lipschitz continuous, cf. Thm. 1.4 of Verhulst (1996), it satisfies the following condition: There is a positive constant k such that
for all t. Theorem 6.2 The finite-time Lyapunov exponent becomes constant along trajectories for large integration times T. PROOF. We compare the value of the finite-time Lyapunov exponent computed at two different points of the same trajectory. Without loss of generality, we assume that the initial time is t0 = 0. Let
for some arbitrary, but fixed,
where we have used properties of the flow map given in Eq. (3) and the maximum exponential stretching hypothesis of Eq. (26). Similarly,
so we have
Therefore
Taking the limit as
which implies
■ The following Corollary provides a bound on the variation of
PROOF. From Eq. (28)
As a result,
Taking the (spatial) derivative of this equation yields
assuming that
which is reasonable since
■ Let
Lemma 6.1
PROOF. This result holds due to the symmetry of mixed partials. For example,
from
■ PROOF. From Def. 5.1, SR2 implies that
since by definition the two vectors are orthogonal, where
■ PROOF.
Developing v in
the orthonormal basis
A direct computation of
■ PROOF. Everywhere in U, L is
smooth and the gradient
■
PROOF. Take x on
the LCS at time t, i.e.
Therefore,
Now expanding
From Eqs. (19) and (38) we have
Since y is
on the LCS at time
Hence, we get the desired result, since
■ We now have all the precursors to prove Thm. 6.1, which we have restated below for convenience. PROOF. Lemma 6.3 gives
Applying Cor. 6.2 and the chain rule for the derivative gives
Using Cor. 6.1 in Eq. (44) gives
and the result follows by noticing that for L = 0,
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Page created 04-15-2005, Last updated 04-15-05, Copyright © 2005, All Rights Reserved.