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Assignment 5-1-2
Principles of Gas Turbine Operation Review
| Question | Answer |
|---|---|
| 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. |