Q1. What is the primary function of a gas turbine engine in aircraft?
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Q2. In a turbofan engine, most of the thrust is produced by:
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Q3. The Brayton cycle is the thermodynamic cycle of:
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Q4. The compressor in a gas turbine engine is used to:
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Q5. Which of the following is a type of gas turbine engine?
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Q6. What is the main disadvantage of turbojet engines compared to turbofans?
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Q7. Afterburners are primarily used in:
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Q8. What protects turbine blades from extreme heat?
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Q9. The efficiency of a gas turbine engine increases with:
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Q10. Which section of a gas turbine is prone to compressor stall?
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Q11. Specific fuel consumption (SFC) of a turbofan engine is generally:
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Q12. Which gas turbine component directly extracts energy from hot gases?
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Q13. The bypass ratio of a turbofan engine is defined as:
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Q14. In jet engines, thrust is produced according to:
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Q15. Which type of gas turbine is widely used in helicopters?
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Q16. Surge in a compressor is characterized by:
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Q17. The nozzle in a gas turbine engine converts:
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Q18. What is the purpose of the combustor in a gas turbine engine?
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Q19. Which factor limits the maximum operating temperature of a gas turbine?
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Q20. The thrust-to-weight ratio of a gas turbine engine is important because:
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