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Fluid Mechanics and Thermodynamics of Turbomachinery, 5e

Fluid Mechanics and Thermodynamics of Turbomachinery, 5e

Fluid Mechanics and Thermodynamics of Turbomachinery, 5e

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xx List <strong>of</strong> Symbols<br />

M Mach number<br />

m mass, molecular “weight”<br />

N rotational speed, axial length <strong>of</strong> diffuser<br />

NS specific speed (rev)<br />

power specific speed (rev)<br />

NSP<br />

NSS<br />

suction specific speed (rev)<br />

n number <strong>of</strong> stages, polytropic index<br />

P power<br />

p pressure<br />

pa atmospheric pressure<br />

vapour pressure<br />

pv<br />

pw<br />

rate <strong>of</strong> energy loss<br />

Q heat transfer, volume flow rate<br />

q dryness fraction<br />

R reaction, specific gas constant, tip radius <strong>of</strong> a blade, radius <strong>of</strong><br />

slipstream<br />

Re Reynolds number<br />

reheat factor<br />

RH<br />

Ro<br />

universal gas constant<br />

r radius<br />

S entropy, power ratio<br />

s blade pitch, specific entropy<br />

T temperature<br />

t time, thickness<br />

U blade speed, internal energy<br />

u specific internal energy<br />

V, v volume, specific volume<br />

W work transfer<br />

DW specific work transfer<br />

w relative velocity<br />

X axial force<br />

x, y, z Cartesian coordinate directions<br />

Y tangential force, actual tangential blade load per unit span<br />

Yid ideal tangential blade load per unit span<br />

Yk tip clearance loss coefficient<br />

Yp pr<strong>of</strong>ile loss coefficient<br />

YS net secondary loss coefficient<br />

Z number <strong>of</strong> blades, Ainley blade loading parameter<br />

a absolute flow angle<br />

b relative flow angle, pitch angle <strong>of</strong> blade<br />

G circulation<br />

g ratio <strong>of</strong> specific heats<br />

d deviation angle<br />

e fluid deflection angle, cooling effectiveness, drag–lift ratio

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