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