GATE AE · 2019 · AE
Question 29: Engine Performance
Give it a try, then reveal the answer to check your work.
Question 29
AEMCQ2 marksNeeds review
In a turbot engine, the compressor outlet temperature increases with decrease efficiency of the compressor. If the turbine inlet temperature remains constant, with decreasing efficiency of the compressor, the thrust specific fuel consumption of the engine
Your answerChoose one option.
Log in to check the answer
You can attempt this question now. Sign in to view the answer key, explanations and discussion.Log in to check answerEXPLORE & PRACTISE
Paper and topic context
See where this question comes from and choose what to practise next.
2019AE
GATE AE 2019 · Paper 1
Aerospace Engineering · Original paper archive
- Section
- Aerospace Engineering
- Question type
- Multiple choice (MCQ)
- Marks
- 2 marks
Practise related topics
Explore more previous year questions using this question’s imported topic tags.
aerospace engineering
GATE AE previous year questions
aerodynamics
GATE AE previous year questions
flight mechanics
GATE AE previous year questions
engine performance
GATE AE previous year questions
Comments
Ask a question, share your approach, or help someone understand.
Log in to view the discussion
You’re not logged in. Log in or create an account to see discussions and add comments.