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Synthetic Inflow Condition for Large Eddy Simulation (Synthetic - KTH

Synthetic Inflow Condition for Large Eddy Simulation (Synthetic - KTH

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3.2.3 Higher order statistics<br />

CHAPTER 3. THE SYNTHETIC EDDY METHOD<br />

Moreover in order to understand better the behavior of the signal, higher order<br />

moments as the skewness and the flatness, will be computed which will allow us to<br />

check afterwards the validity of the SEM implementation.<br />

3.2.3.1 Skewness<br />

To express the final equations of these statistics we have to start with another<br />

<strong>for</strong>mulation of the SEM velocity fluctuations by rearranging Eq. (3.3) as<br />

u ′<br />

i(x, t) = 1<br />

√ N<br />

with, X (k)<br />

i<br />

N�<br />

k=1<br />

X (k)<br />

i<br />

= aijε k j fσ(x − x k )<br />

(3.20)<br />

Xk i being independent random variables following the same distribution, the<br />

central limit theorem can be applied. This states that when N tends towards infinity,<br />

the probability density function of u ′<br />

i (x, t) tends towards a Normal distribution<br />

N(µi, σ 2 i ) of mean µi = 〈X k i 〉 and of variance σ2 i = 〈(Xk i )2 〉. In this method it<br />

would mean, when the number of eddies N tends towards infinity, the signature of<br />

each eddy in the final synthetic signal becomes more faint and the final signal tends<br />

toward a universal Gaussian state.<br />

From there we can thus express the skewness of the velocity signal using Eq.(3.20).<br />

Sui = 〈u′ 3<br />

i 〉<br />

〈u ′ = 2<br />

i 〉 3/2<br />

which is shown to be zero<br />

1<br />

(NRii) 3/2<br />

��<br />

N�<br />

X<br />

k=1<br />

(k)<br />

�3�<br />

i<br />

Sui<br />

Actually using the multinomial theorem,<br />

(x1 + x2 + ... + xm) n =<br />

�<br />

k1,k2,...,km<br />

(3.21)<br />

= 0 (3.22)<br />

n!<br />

k1!k2!...km! xk1 1 xk2 2 ...xkm m<br />

(3.23)<br />

with � ki = n <strong>for</strong> any positive integer m and any non-negative integer n, we obtain,<br />

28

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