NAVWEPS 00-80T-80 
AIRPLANE PERFORMANCE 
PRIMARY 
COMBUSTION 
AIR7 
TYPICAL COMBUSTION CHAMBER 
SECONDARY Al R 
OR COOLING FLOW 
FUEL 
SPRAY 
NOZZLE 
DISCHARGE 
TO TURBINE 
NOZZLES 
COMBUsTlON 
NUCLEUS 
TURBINE SECTION 
TUR’BINE NOZZLE VANES 
r / 11 TmaiNt BLADES 
TURBINE WHEEL SHAFT 
TURBIhE BLADING 
(STATIONARY) 
(ROTATING) TURBINE BLADES 
Figure 2.8. Combustion Chamber and Turbine Components 
112