This test is to help prepare you for your CDC EOC. This not to be used as a replacement for your books.
Bernoulli's principle
Newton's first law of motion
Newton's second law of motion
Newton's third law of motion
Elbow
Straight
Divergent
Convergent
Bernoulli's principle
Newton's first law of motion
Newton's second law of motion
Newton's third law of motion
Energy
Inertia
Friction
Potential
Turbine
Diffuser
Compressor
Combustion
Accelerating a large mass of air by a small amount
Moving a small quantity of air through a large velocity change.
Using the same working fluid for propulsive force as that used within the engine
Using only the energy expended through the exhaust nozzle to propel the aircraft forward
Brake
Indicated
Frictional
Equivalent shaft
10,500
15,500
18,500
40,000
Potentiometer
Psychrometer
Pyrometer
Barometer
Increases pressure
Decreases pressure
Has no effect on pressure
Results in pressure fluctuations
P&D valve
Fuel pump
Fuel control
Fuel nozzles
Flameholder
Combustion chamber
Turbine wheel blades
Turbine stator
Diffuser
Jet nozzle
Combustion chamber
Turbine stator(nozzle diaphragm)
Turbo
Turbine
Exhaust
Diffuser
Sliding-vane air compressors
Piston pump air compressors
Roots air compressors
Turbo-superchargers
Rotational and centrifugal
Rotational and tangential
Tangential and centrifugal
Tangential and radial
Has two matching plates
Has a lightweight design
Is a forged single unit
Is constructed in rows of blades and stators
Act as a vibation damper
Allow cooling air to the turbine
Provide a passage for lubricating oil
Provide a passage for the main fuel supply
Direct air and increase pressure
Direct hot gases rearward
Increase backup pressure
Prolong compressor life
Starter
Fuel pump
Fuel control
Low-pressure turbine
Gold plating on the plug
Split electrode on the plug
Ceramic coating on the plug
Directing air around the plug
Cool the burner surfaces
Operate pneumatic accessories
Decrease the mass of exhaust gases
Increase air in compressor section
Returned to the fuel control by tubes
Drained overboard by a drain system
Burned on the next start attempt
Allowed to evaporate
Fuel nozzle
Transition liner
Combustion chamber outer case
Combustion chamber cross over tubes
Pressure-atomizing
Fuel-blasting
Fuel ejector
Fuel tube
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