#1. The basic gas turbine engine is divided into two main sections: the cold section and the hot section.
The hot section includes the combustor, turbine, and exhaust.
The hot section includes the combustor, inlet, and exhaust.
#2. At what point in an axial flow turbojet engine will the highest gas pressures occur?
Within the burner section
At the compressor outlet
#3. A gas turbine engine comprises which three main sections?
Compressor, diffuser, and stator
Turbine, compressor, and combustion
#4. Standard sea level pressure is...
29.92 inches Hg
29.00 inches Hg
#5. In a gas turbine engine, turbine section...
velocity decreases and pressure increases
velocity increases and pressure decreases
#6. If an electrical de-icing system is operating, thrust will...
#7. A pitot intake is divergent from front to rear because it...
speeds up the air before it hits the compressor face
produces the maximum amount of ram compression
#8. Intake air turbulence...
increases the efficiency of the compressor
decreases the efficiency of the compressor
#9. What are the two main functional components in a centrifugal compressor?
Turbine and compressor
Impeller and diffuser
#10. Which two elements make up the axial flow compressor assembly?
Rotor and stator
Stator and diffuser