Podcast
Questions and Answers
What is the formula that represents the relationship between force, pressure, and area in a gas turbine engine?
What is the formula that represents the relationship between force, pressure, and area in a gas turbine engine?
- F = A/P
- F = P·A (correct)
- F = P/A
- F = P + A
Which statement best describes how thrust is generated in a gas turbine engine?
Which statement best describes how thrust is generated in a gas turbine engine?
- Thrust relies on the pressure difference between stages of the compressor.
- Thrust is generated from the reaction to the mass flow of accelerated gases. (correct)
- Thrust is produced solely by the velocity of the exhaust gases.
- Thrust results from energy creation in the combustion chamber.
In the context of a gas turbine engine, work is defined as:
In the context of a gas turbine engine, work is defined as:
- The output of thrust generated by the turbine.
- The transfer of energy to a body by a force that moves the body. (correct)
- The transfer of energy without the application of force.
- The energy lost in heat forms during combustion.
What role does atmospheric air play in a gas turbine engine?
What role does atmospheric air play in a gas turbine engine?
Which physical principle is essential for understanding jet propulsion?
Which physical principle is essential for understanding jet propulsion?
Which components are primarily involved in the creation of useful work at the turbine wheel in a gas turbine?
Which components are primarily involved in the creation of useful work at the turbine wheel in a gas turbine?
What does the term 'mass flow of gases' refer to in a gas turbine engine?
What does the term 'mass flow of gases' refer to in a gas turbine engine?
What is one of the primary functions of nozzle guide vanes in a gas turbine engine?
What is one of the primary functions of nozzle guide vanes in a gas turbine engine?
What is the primary factor that differentiates velocity from speed?
What is the primary factor that differentiates velocity from speed?
According to Bernoulli's Principle, what remains constant throughout a moving fluid column?
According to Bernoulli's Principle, what remains constant throughout a moving fluid column?
In a gas turbine engine, what role does burning fuel play in relation to air flow?
In a gas turbine engine, what role does burning fuel play in relation to air flow?
How is momentum defined in the context of physics as described in the content?
How is momentum defined in the context of physics as described in the content?
What occurs to the pressure of a fluid as its velocity increases in a duct according to Bernoulli's Principle?
What occurs to the pressure of a fluid as its velocity increases in a duct according to Bernoulli's Principle?
When analyzing the flow of fluid in a duct, what happens to the product of velocity and pressure at different points in the duct?
When analyzing the flow of fluid in a duct, what happens to the product of velocity and pressure at different points in the duct?
What is a key characteristic that defines speed?
What is a key characteristic that defines speed?
Which of the following statements about kinetic and potential energy is true as per Bernoulli's Principle?
Which of the following statements about kinetic and potential energy is true as per Bernoulli's Principle?
What is the primary principle behind all aircraft propulsion?
What is the primary principle behind all aircraft propulsion?
Which ancient device is credited with the concept of thrust similar to modern engines?
Which ancient device is credited with the concept of thrust similar to modern engines?
How does aerodynamic action produce thrust in an aircraft?
How does aerodynamic action produce thrust in an aircraft?
What is a characteristic feature of jet reaction engines?
What is a characteristic feature of jet reaction engines?
What role did the Chinese play in the development of propulsion systems?
What role did the Chinese play in the development of propulsion systems?
What mechanism does an engine use to achieve thrust through aerodynamic action?
What mechanism does an engine use to achieve thrust through aerodynamic action?
Which of the following statements best describes the operation of a rocket engine?
Which of the following statements best describes the operation of a rocket engine?
What comparison is made to explain the principle of thrust generation in jet propulsion?
What comparison is made to explain the principle of thrust generation in jet propulsion?
Which event does the Brayton cycle share with the Otto cycle?
Which event does the Brayton cycle share with the Otto cycle?
What is a primary characteristic of the Brayton cycle compared to the Otto cycle?
What is a primary characteristic of the Brayton cycle compared to the Otto cycle?
During which phase of the Brayton cycle does the volume of the air decrease?
During which phase of the Brayton cycle does the volume of the air decrease?
How does the process of energy addition in the Brayton cycle differ from that in the Otto cycle?
How does the process of energy addition in the Brayton cycle differ from that in the Otto cycle?
At which point does the pressure remain relatively constant during the Brayton cycle?
At which point does the pressure remain relatively constant during the Brayton cycle?
What is the main effect of adding heat energy in the combustion chamber of the Brayton cycle?
What is the main effect of adding heat energy in the combustion chamber of the Brayton cycle?
At what stage does the air exit the compressor in the Brayton cycle?
At what stage does the air exit the compressor in the Brayton cycle?
Which aspect of the Brayton cycle distinguishes it from engines with reciprocating cycles like the Otto cycle?
Which aspect of the Brayton cycle distinguishes it from engines with reciprocating cycles like the Otto cycle?
What occurs to the air as it moves from point A to point D in the turbine?
What occurs to the air as it moves from point A to point D in the turbine?
What is a key advantage of gas turbines over reciprocating engines?
What is a key advantage of gas turbines over reciprocating engines?
Which part of the gas turbine is predominantly responsible for converting thermal energy into mechanical energy?
Which part of the gas turbine is predominantly responsible for converting thermal energy into mechanical energy?
What is a characteristic of air as it passes through the compressor section of a gas turbine?
What is a characteristic of air as it passes through the compressor section of a gas turbine?
What is the main function of the combustion chamber in a gas turbine?
What is the main function of the combustion chamber in a gas turbine?
How does the design of reciprocating engines typically affect their weight compared to gas turbines?
How does the design of reciprocating engines typically affect their weight compared to gas turbines?
What happens to the velocity of the air during the expansion process in the turbine?
What happens to the velocity of the air during the expansion process in the turbine?
In a gas turbine engine, which phase occurs immediately after combustion?
In a gas turbine engine, which phase occurs immediately after combustion?
What is the engine pressure ratio (EPR) when turbine discharge pressure is 28.52 psia and compressor inlet pressure is 14.7 psia?
What is the engine pressure ratio (EPR) when turbine discharge pressure is 28.52 psia and compressor inlet pressure is 14.7 psia?
Which station numbers does the Pratt & Whitney Company use to identify the engine pressure ratio tap-off points in dual-spool engines?
Which station numbers does the Pratt & Whitney Company use to identify the engine pressure ratio tap-off points in dual-spool engines?
When an aeroplane is flying at 375 miles per hour, each pound of thrust equates to how many horsepower?
When an aeroplane is flying at 375 miles per hour, each pound of thrust equates to how many horsepower?
If the speed of the aeroplane is doubled, what happens to the horsepower produced by each pound of thrust?
If the speed of the aeroplane is doubled, what happens to the horsepower produced by each pound of thrust?
What is the static thrust power (ESHP) formula component associated with the speed of the aircraft?
What is the static thrust power (ESHP) formula component associated with the speed of the aircraft?
In the context of thrust power, which of the following is NOT a unit of measurement for power?
In the context of thrust power, which of the following is NOT a unit of measurement for power?
How is the ESHP adjusted when the thrust produced by the propeller is considered?
How is the ESHP adjusted when the thrust produced by the propeller is considered?
Which equation represents the relationship between thrust and speed for computing power in jet propulsion?
Which equation represents the relationship between thrust and speed for computing power in jet propulsion?
Flashcards
Work
Work
The transfer of energy to a body by the application of a force that moves the body in the direction of the force.
Gas Turbine Engine Function
Gas Turbine Engine Function
The mass-flow of gases referred to is atmospheric air which is compressed and accelerated in the gas turbine engine to create useful work at the turbine wheel and ultimately, thrust. The thrust is created from either pure reaction to the flowing.
Physics in Jet Propulsion
Physics in Jet Propulsion
Physical principles that govern the action of mass or matter, essential for understanding the relationship of gases and the turbo-machinery within a gas turbine engine.
Pressure
Pressure
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Volume
Volume
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Atmospheric Pressure
Atmospheric Pressure
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Velocity
Velocity
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Acceleration
Acceleration
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Speed
Speed
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Momentum
Momentum
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Bernoulli's Principle
Bernoulli's Principle
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Gas Turbine Engine
Gas Turbine Engine
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Thrust
Thrust
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Kinetic Energy
Kinetic Energy
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Potential Energy
Potential Energy
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Aerodynamic action
Aerodynamic action
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Jet reaction
Jet reaction
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Newton's 3rd law in propulsion
Newton's 3rd law in propulsion
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Brayton Cycle
Brayton Cycle
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Compression
Compression
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Expansion
Expansion
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Combustion
Combustion
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Expansion Through Turbine
Expansion Through Turbine
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Air Intake
Air Intake
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Exhaust
Exhaust
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Heat Addition
Heat Addition
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Turbine
Turbine
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Engine Pressure Ratio (EPR)
Engine Pressure Ratio (EPR)
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Equivalent Static Shaft Horsepower (ESHP)
Equivalent Static Shaft Horsepower (ESHP)
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Thrust Power
Thrust Power
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Engine Station Numbering
Engine Station Numbering
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Shaft Horsepower (SHP)
Shaft Horsepower (SHP)
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Propeller Efficiency
Propeller Efficiency
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Newton's Third Law of Motion
Newton's Third Law of Motion
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Study Notes
15.1 Fundamentals
- Physics is fundamental to understanding gas turbine engines.
- Force is the capacity to do work. Work is done when a force moves an object through distance. Acceleration is change in velocity over time.
- Thrust is proportional to both mass and acceleration.
- Mass is the amount of matter in an object.
- Force is a vector having both magnitude and direction.
- Work is the transfer of energy. Kinetic energy is energy of motion. Potential energy is energy due to position or condition.
- Power is the rate at which work is done.
- Units of measurement: Force (N), Pressure (N/m²), Area (m²), Work (Joules), Distance (m), Time (s), Power(Watts).
15.2 Engine Performance
- Thrust is a measure of the output of a turbojet or turbofan engine, not appropriate to use horsepower.
- Momentum is the impulse imparted to the air, fuel and combustion products flowing through, either adding to or subtracting from the total.
- Net thrust considers change in momentum of air/fuel and pressure difference at nozzle (exit).
- Gross thrust considers nozzle pressure, exhaust momentum.
- Thrust is influenced by factors such as altitude, airspeed and temperature affecting the flow of air through the engine.
- Factors affecting thrust include mass airflow, exhaust nozzle jet velocity, and airspeed.
15.3 Inlet
- Air inlet ducts direct air into the engine.
- Subsonic and supersonic inlets have different designs.
- Ice and debris protection is crucial for inlets.
15.4 Compressors
- Compressors increase air pressure.
- Types include centrifugal and axial flow compressors.
- Compressor design features include guide vanes, stator vanes and converging airflow path.
- Axial-flow compressors are categorized by single spool, dual spool, and triple spool.
15.5 Combustion Section
- Principles of operation: Gas turbine combustion principles (how power is created).
- Multiple-can, Can-Annular, Annular, Reverse-Flow annular combustors.
15.6 Turbine Section
- Turbine elements, design and construction, and failure analysis.
- Materials, Nozzle Guide Vanes, Turbine Discs and Compressor-Turbine Matching are key elements in turbine section components.
15.7 Exhaust
- Turbine engine exhaust and its associated noise suppressors and thrust reversers.
Types of Gas Turbine Engines
- Reciprocating engines have limitations in power, weight and maintenance compared to gas turbines. Gas turbines have a higher efficiency and fewer moving parts.
- Ramjet, pulse jet, turbojet, turboprop and turbofan engines.
- Ramjet and pulse jet engines are simple, but limited in speed capability.
Brayton Cycle
- The Brayton cycle describes the thermodynamic cycle of a gas turbine engine.
- Constant pressure cycle. Similar events occur at different times & locations from the constant volume Otto cycle.
- Air enters the compressor, is compressed, then heated, then passes through a turbine, and finally to the nozzle.
- Flow of air is from inlet to compressor, then to combustion chamber, then to turbine and finally to exhaust.
Turbine Engine Terms and Definitions
- The engine is divided into "cold section" and "hot section".
- Stations are designated numerically to enable accurate identification.
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