AGTE FUNDAMENTALS

Quiz
•
Science
•
University
•
Hard
Adolfo Cruz
Used 8+ times
FREE Resource
10 questions
Show all answers
1.
MULTIPLE CHOICE QUESTION
1 min • 1 pt
When gases pass through a convergent duct their:
A) velocity and temperature increase and their pressure decreases
B) their velocity increases and their temperature and pressure decrease
C) their velocity decreases and their temperature and pressure increase
D) they expand adiabatically
2.
MULTIPLE CHOICE QUESTION
1 min • 1 pt
Select the correct order of best propulsive efficiency, from low to high airspeed.
A) High bypass ratio turbojet, Low bypass ratio turbojet, Pure turbojet, Turboprop
B) Low bypass ratio turbojet, Pure turbojet, Turboprop, High bypass ratio turbojet
C) Pure turbojet, Turboprop, High bypass ratio turbojet, Low bypass ratio turbojet
D) Turboprop, High bypass ratio turbojet, Low bypass ratio turbojet, Pure turbojet
3.
MULTIPLE CHOICE QUESTION
1 min • 1 pt
The highest pressure in a gas turbine engine occurs:
A) between the compressor and the combustion chamber
B) in the combustion chamber
C) in the jet pipe
D) at the P1 probe
4.
MULTIPLE CHOICE QUESTION
1 min • 1 pt
In a turbofan engine, the fan speed is controlled by:
A)
a reduction gear
B)
a wastegate
C) the turbine
D) varying the pitch
5.
MULTIPLE CHOICE QUESTION
1 min • 1 pt
In a High Bypass Ratio engine:
A) all of the air goes through both the low and high pressure compressors
B) not all the air goes through the high pressure compressor
C) not all the air goes through the low pressure compressor
D) all the air goes through the high pressure compressor
6.
MULTIPLE CHOICE QUESTION
1 min • 1 pt
Modular construction:
A) is only used on turboprop engines
B) cannot be used on high ratio engines
C) has a weight saving function
D) enables malfunctioning sections of the engine to be changed without changing the whole engine
7.
MULTIPLE CHOICE QUESTION
1 min • 1 pt
The Bypass Ratio of an engine is the ratio of:
A) primary air to tertiary air
B) cold stream air to that flowing through the hot core of the engine
C) exhaust gas pressure to air intake pressure
D) primary air to secondary air
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