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Assignment 5-1-2

Principles of Gas Turbine Operation Review

QuestionAnswer
1. Describe the relationship between pressure and velocity in a closed system Together they make up total pressure
2. How does subsonic airflow react through a convergent opening? A divergent opening? Convergent: velocity increase and pressure decreases. Divergent: velocity decreases and pressure increase.
3. How does supersonic airflow react through a convergent opening? A divergent opening? Convergent: velocity decrease and pressure increase. Divergent: velocity increases and pressure decreases.
4. What happens to the airflow as it passes through a nozzle? A diffuser? Nozzle: velocity increases and pressure decreases. Diffuser: velocity decreases and pressure increases.
5. What are the three sections of a gas generator? Compressor, burner, turbine.
6. How does a gas turbine engine produce thrust? By rapidly compressing, heating and accelerating a large (mass) of air and fuel?
7. What cycle explains the movement of air through a gas generator? Brayton cycle. Suck, Squeeze, Bang, Blow
8. What happens to the velocity of the gasses as they pass through the compressor section? Compressor: Remains fairly constant. Burner and turbine: increases
9. What is gross thrust? Thrust measured at exhaust at standard day conditions 29.92 and 15 decrease celcios.
10. What is net thrust? Thrust measured under normal flight conditions.
11. When are gross thrust and net thrust equal? When aircraft is in static position and standard day conditions.
12. What affects the density of the air mass? Temperature, pressure, and altitude.
13. What happens to thrust when air density decrease? Thrust decreases.
14. What happens to thrust when air temperature increase? Thrust decreases.
15. What happens to thrust when air pressure decrease? Thrust decrease.
16. What is the relationship between pressure and temperature as altitude increase? Temperature and pressure decrease with an over all decrease in thrust.
17. What is the optimum altitude and why? Approximately 36,00 feet and temperature remains isothermal.
18. How does airspeed and the ram effect changes the amount of thrust produced at subsonic and supersonic speeds? Airspeed increase without ram effect cause thrust to decrease. Airspeed increase with ram effect causes thrust to remain relatively constant at subsonic speeds and increased greatly at supersonic speeds.
Created by: Rudyrm
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