M a

Mach number

R E

Eulerian correlation coefficient

R L

Lagrangian correlation coefficient

R i j

two-point correlation coefficient of u i and ω j ( i , j = 1 , 2 , 3 )

R e

Reynolds number

R e τ

Reynolds number defined with the friction velocity

R e θ

Reynolds number defined with the momentum loss thickness of turbulent boundary layer

t

time (s)

U

mean velocity (m∙s−1)

U C

propagation speed (m∙s−1)

( u 1 , u 2 , u 3 ) or ( u , v , w )

velocity components in the streamwise, wall normal and spanwise directions, respectively (m∙s−1)

( x 1 , x 2 , x 3 ) or ( x , y , z )

coordinates in the streamwise, wall normal and spanwise directions, respectively (m)

δ

thickness of turbulent boundary layer (m)

ν

kinematic viscosity (m2∙s−1)

ϕ or ψ

fluctuations of a variable or component

( ω 1 , ω 2 , ω 3 ) or ( ω x , ω y , ω z )

vorticity components in the streamwise, wall normal and spanwise directions, respectively (s−1)

Subscripts

i or j

coordinate indices, ( i , j = 1 , 2 , 3 )

r

reference point

x, y, z

coordinate indices for the streamwise, wall normal and spanwise directions, also represented by 1, 2 and 3, respectively

Superscripts

+

normalized with wall units