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Physics Fundamentals for Jet Propulsion
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Physics Fundamentals for Jet Propulsion

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Questions and Answers

What is the unit of power in the formula P = F × t?

  • ft-lb/min
  • lb-ft/s
  • lb-ft/min (correct)
  • lb-ft
  • What is the difference between displacement and distance?

  • Displacement is always less than distance.
  • Displacement is a scalar quantity and distance is a vector quantity.
  • Displacement is a vector quantity and distance is a scalar quantity. (correct)
  • Displacement is always greater than distance.
  • Which of the following is a scalar quantity?

  • Speed (correct)
  • Displacement
  • Velocity
  • Acceleration
  • What is the unit of the force in the formula P = F × t?

    <p>lb</p> Signup and view all the answers

    Why does accelerating a 1500-kg vehicle over 1/4 mi in 7 s require more power than doing so in 5 min?

    <p>Because the time is shorter</p> Signup and view all the answers

    What is the main difference between velocity and speed?

    <p>Velocity is a vector quantity and speed is a scalar quantity.</p> Signup and view all the answers

    What is the characteristic of air flow in a low-bypass engine?

    <p>The airflow is divided approximately into two halves between the fan and the compressor.</p> Signup and view all the answers

    What is the purpose of mixing the hot and cold gas streams in a mixed exhaust engine?

    <p>To decrease the noise pollution</p> Signup and view all the answers

    What is the fan ratio of a high-bypass engine?

    <p>4:1 to &lt; 9:1</p> Signup and view all the answers

    What is the characteristic of a non-mixed exhaust engine?

    <p>The hot and cold gas streams are not mixed before entering the atmosphere</p> Signup and view all the answers

    What is the purpose of the 'cold gas stream' in a low-bypass engine?

    <p>To generate thrust</p> Signup and view all the answers

    What is the design requirement for a high-bypass engine?

    <p>A large-diameter fan is required</p> Signup and view all the answers

    What is the primary mechanism used by a turbojet engine to produce thrust?

    <p>The acceleration of airflow throughout the engine</p> Signup and view all the answers

    At what speed range is the turbojet or turbofan engine most widely used?

    <p>From 450 mph up</p> Signup and view all the answers

    What is the main advantage of the turbofan engine over the turbojet engine?

    <p>Ability to use higher turbine temperatures without increasing jet velocity</p> Signup and view all the answers

    What is the purpose of the turbine wheels in a turbojet engine?

    <p>To drive the compressor blades</p> Signup and view all the answers

    What is the primary difference between a turbojet engine and a turbofan engine?

    <p>The presence of a bypass fan</p> Signup and view all the answers

    What is the main reason why the turbojet engine has been largely replaced by the turbofan engine?

    <p>Less efficient for subsonic flight</p> Signup and view all the answers

    What percentage of airflow accelerated by the fan rotor blades is ducted past the core engine?

    <p>Up to 90%</p> Signup and view all the answers

    What is the purpose of the duct in a ducted fan engine?

    <p>To reduce airflow separation from the blades at speeds over Mach 1</p> Signup and view all the answers

    Why do high-bypass engines and ducted fan engines produce more fan thrust than low-bypass engines?

    <p>Because they suffer less loss through skin friction with their short ducts</p> Signup and view all the answers

    What is the purpose of the engine station system in maintenance manuals?

    <p>To identify the position of a component or fitting along the engine's axis</p> Signup and view all the answers

    What determines the number of designated engine stations in an engine?

    <p>The engine's complexity</p> Signup and view all the answers

    What is the name of the engine design where the fan is arranged behind the turbine and powered by a shaft from the turbine?

    <p>Aft fan</p> Signup and view all the answers

    What is the primary concern of gas turbine engines?

    <p>Thrust produced</p> Signup and view all the answers

    What is the formula to calculate force in gas turbine engines?

    <p>F = P × A</p> Signup and view all the answers

    What is the unit of measurement for force in gas turbine engines?

    <p>Pounds</p> Signup and view all the answers

    What is the definition of force in physics?

    <p>The capacity to do work or produce acceleration</p> Signup and view all the answers

    What is the pressure measurement across the opening of a jet tailpipe in the worked example?

    <p>6 psi above ambient</p> Signup and view all the answers

    What is the primary application of the physics principles in gas turbine engines?

    <p>To compress and accelerate atmospheric air</p> Signup and view all the answers

    Study Notes

    Physics Fundamentals

    • Physics principles govern the action of mass or matter in jet propulsion.
    • Understanding the relationships between gases and turbo-machinery is crucial for gas turbine engines.

    Force and Thrust

    • Force is the capacity to do work or the tendency to produce work, and is a vector quantity.
    • Force can be measured in pounds.
    • Thrust is the force produced by a gas turbine engine, rated in pounds of thrust.
    • Formula for force: F = P × A, where F is force, P is pressure, and A is area.

    Work and Power

    • Power is measured in horsepower or kilowatts in reciprocating engines, but gas turbine engines are concerned with thrust.
    • Thrust is often rated in combination with shaft horsepower in turboprop applications.

    Displacement and Distance

    • Displacement and distance are often used interchangeably, but have distinct definitions.
    • Distance is a scalar quantity, measuring how far an object has traveled.
    • Displacement is a vector quantity, measuring how far an object is from its origin.

    Velocity and Speed

    • Velocity is a vector quantity, having both speed and direction.
    • Speed is a scalar quantity, without direction.

    Bypass Ratios

    • Low-bypass engines have a fan-to-compressor airflow ratio of approximately 1:1.
    • Medium-bypass engines have a ratio of 2:1 or 3:1.
    • High-bypass engines have a ratio of 4:1 to < 9:1.
    • Ultra-high-bypass engines have a ratio of > 9:1.

    Turbojet and Turbofan Engines

    • Turbojet engines use the acceleration of airflow throughout the engine to produce thrust.
    • Turbojet engines are well suited for high-speed, high-altitude operations.
    • Turbofan engines are newer and more popular, with higher propulsive power at higher subsonic cruising speeds.

    Engine Stations

    • Engine stations are numbered locations along the axis line of the engine, following the gas path.
    • Stations refer to specific locations such as the compressor inlet, compressor outlet, and turbine inlet and outlet.

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    Description

    Understanding the physical relationships between gases and turbo-machinery in a gas turbine engine, focusing on atmospheric air compression and acceleration.

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