
Gas Turbine Engine Quiz 2

Quiz
•
Physics
•
University
•
Medium

Peter Spahr
Used 1+ times
FREE Resource
15 questions
Show all answers
1.
MULTIPLE CHOICE QUESTION
30 sec • 1 pt
What is the name of the thermodynamic cycle used by a gas turbine engine?
Otto cycle
Rankine cycle
Diesel cycle
Brayton cycle
2.
MULTIPLE CHOICE QUESTION
30 sec • 1 pt
What is the basic difference between the Otto cycle and the Brayton cycle?
The Brayton cycle uses a constant-pressure thermodynamic cycle, while the Otto cycle uses a constant-volume thermodynamic cycle
The events occur at different times in the Otto cycle, but at the same time in the Brayton cycle
The events occur at the same location in the Otto cycle, but at different locations in the Brayton cycle
The Otto cycle uses a constant-pressure thermodynamic cycle, while the Brayton cycle uses a constant-volume thermodynamic cycle
3.
MULTIPLE CHOICE QUESTION
30 sec • 1 pt
What is the primary measure of the propulsive force developed by a turbojet or turbofan engine?
Thrust
Horsepower
RPM
Torque
4.
MULTIPLE CHOICE QUESTION
30 sec • 1 pt
What is the formula for calculating the momentum of air and fuel leaving the engine?
WaW₁/g
Fn = Wa (V₂ - V₁) + Wf (V₂) + Aj (P2 - Pam)/g
(Wa+Wf)/g
V₁ +0
5.
MULTIPLE CHOICE QUESTION
30 sec • 1 pt
What is the effect of airspeed on the net thrust produced by a turbojet or turbofan engine?
Net thrust remains constant regardless of airspeed
Net thrust decreases with an increase in airspeed
Net thrust is not affected by airspeed
Net thrust increases with an increase in airspeed
6.
MULTIPLE CHOICE QUESTION
30 sec • 1 pt
What is the effect of air temperature on the thrust produced by a gas turbine engine?
Thrust increases linearly with air temperature
As air temperature increases, thrust increases
As air temperature increases, thrust decreases
Air temperature has no effect on thrust
7.
MULTIPLE CHOICE QUESTION
30 sec • 1 pt
What is the effect of air pressure on the thrust produced by a gas turbine engine?
As air pressure increases, thrust increases
As air pressure increases, thrust decreases
Thrust increases linearly with air pressure
Air pressure has no effect on thrust
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