GATE AE · 2024 · AE
Question 43: Compressible Flows
Give it a try, then reveal the answer to check your work.
Question 43
AEMCQ2 marksNeeds review
Shock structures for flow at three different Mach numbers over a given wedge are shown in the figure below. Assuming that only the weak shock solutions are possible for the attached oblique shocks, which one of the following options is TRUE?
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.
2024AE
GATE AE 2024 · 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
compressible flows
GATE AE previous year questions
oblique shocks
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.