GATE AE · 2020 · AE
Question 27: Compressible Flows
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Question 27
AEMCQ2 marksNeeds review
A wedge shaped airfoil is placed in a supersonic flow as shown in the figure (not to scale). The corners of the wedge are at
,
,
, respectively. Which one of the following represents the correct static pressure profiles along
and
? 
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2020AE
GATE AE 2020 · Paper 1
Aerospace Engineering · Original paper archive
- Section
- Aerospace Engineering
- Question type
- Multiple choice (MCQ)
- Marks
- 2 marks
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