A turbine's operating reliability can be described as something

Ensured by the manufacturer by fully testing and monitoring the buildup

The Brayton Cycle means

Combustion is constant/continuous

comparison between engine exhaust pressure and compressor inlet pressure

Durability of a Turbine Engine is

The extent to which the engine lasts; operating efficiently between OH's

To every action, there is an equal and opposite reaction

Force produced on an object is proportional to mass times acceleration

A rocket engine has it's own oxidizers on board which allows

The rocket to operate outside the Earth's atmosphere

A turbine's operating flexibility can be described as

Ability of engine to operate seamlessly & achieve performance at all times

The Two Categories of Turbine Engine Types

Non-air-breathing and Air-Breathing Reaction

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PP10-207 Quiz 1

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Questions 17

Answers

1
The Ottoman cycle means
Combustion occurs only during start-up
Combustion is intermittent
Combustion is constant/continuous
2
A turbine's operating reliability can be described as something
Ensured by the manufacturer by fully testing and monitoring the buildup
showing an engine being able to operate seamlessly
3
The Brayton Cycle means
Combustion occurs only during spark
Combustion is constant/continuous
Combustion is intermittent
4
Turboprop and Turboshaft engines produce
Torque
Thrust
5
EPR is the
comparison between engine exhaust temperature and compressor temperature
Comparison between inlet temperature and exhaust temperature
comparison between engine exhaust pressure and compressor inlet pressure
6
Durability of a Turbine Engine is
The extent to which the engine lasts; operating efficiently between OH's
The capability of the engine to operate seamlessly and efficiently
7
Newton's 3rd Law
An object will stay at rest or motion unless acted on by an external force
Motion's opposite reaction is equal to mass times velocity
To every action, there is an equal and opposite reaction
8
Which of these has a Primary and Secondary airflow
Turbojet
Turboshaft
Turboprop
Turbofan
9
Thrust is necessary for flight for all of these reasons except
To increase speed
To increase drag
To increase lift of the wing
10
Pressure energy can be described as
Static Pressure
Dynamic Pressure
11
Newton's 2nd Law
Force produced on an object is proportional to mass times acceleration
To every action, there is an equal and opposite reaction
An object will stay at rest or motion unless acted on by an external force
12
Kinetic energy can be described as
Static Pressure
Dynamic Pressure
13
A rocket engine has it's own oxidizers on board which allows
Allows the rocket to run accessory systems
The rocket to work without fuel
The rocket to operate outside the Earth's atmosphere
14
A turbine's operating flexibility can be described as
Extent to which an Engine lasts, must operate effectively before overhaul
Ability of engine to operate seamlessly & achieve performance at all times
15
The Two Categories of Turbine Engine Types
Non-air-breathing and Air-Breathing Reaction
Air Accelerating, Ram-Air pulsing
Nozzle Discharging, Velocity Propelling
16
Turbofan and Turbojet produce
Thrust
Torque
17
Understanding the laws of Physics for Masses & Gases is required to understand jet propulsion.
True
False

PP10-207 Quiz 1 Flashcards | StudBud