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investigation of a prototype industrial gas turbine combustor using ...

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Q in heat input [J]<br />

Q 1 (8) excitation transition <strong>of</strong> the OH radical<br />

q fuel/air ratio by mass<br />

R characteristic radius [m]<br />

Re Reynolds number<br />

Re 0b post combustion Reynolds number<br />

Rec. recirculated mass flow<br />

R u universal <strong>gas</strong> constant [J/(K mol)]<br />

r radius [m]<br />

r i inner radius [m]<br />

r o outer radius [m]<br />

S specific entropy [J/(kg K)]<br />

S L laminar burning velocity [m/s]<br />

S L0 laminar unstretched burning velocity [m/s]<br />

S T turbulent flame speed [m/s]<br />

St stokes number<br />

S w swirl number<br />

S w,l local swirl number<br />

T temperature [K]<br />

ti time at index i [s]<br />

t 0 integral time scale [s]<br />

t η Kolmogorov time [s]<br />

U velocity [m/s]<br />

u axial velocity [m/s]<br />

u ′ axial rms component <strong>of</strong> the fluctuating velocity [m/s]<br />

u η Kolmogorov velocity [m/s]<br />

V volume [m 3 ]<br />

v ′ transverse fluctuating velocity [m/s]<br />

v ′ vibrational level in the first excited state<br />

v ′′ vibrational level in the ground state<br />

vol. volume [m 3 ]<br />

Wo Wobbe index [MJ/Nm 3 ]<br />

W out work out [J]<br />

w angular velocity component [m/s]<br />

X 2 Π ground electric state in the OH radical<br />

x length in the x direction [m]<br />

xii

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