GATE AE · 2022 · AE
Question 35: Axial Turbines
Give it a try, then reveal the answer to check your work.
Question 35
AENAT1 markNeeds review
In a single stage turbine, the hot gases come out of stator/ nozzle at a speed of 500 m/s and at an angle of 70 degrees with the turbine axis as shown. The design speed of the rotor blade is 250 m/s at the mean blade radius. The rotor blade angle,
, at the leading edge is ________ degrees (round off to one decimal place). 
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.
2022AE
GATE AE 2022 · Paper 1
Aerospace Engineering · Original paper archive
- Section
- Aerospace Engineering
- Question type
- Numerical answer (NAT)
- Marks
- 1 mark
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
axial turbines
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.