GATE AE · 2019 · AE
Question 27: Compressible Flows
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Question 27
AEMCQ2 marksNeeds review
A supersonic flow in a constant area duct at Mach number
encounters a ramp of angle
(see Figure 1). The resulting oblique shock with shock angle
is then reflected from the top wall. For the reflected shock, the turn angle is
and the shock angle is
. 
Use the weak shock solution from the
-
-
plot shown in Figure 2 to choose the correct option from the following. 
Your answerChoose one option.
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2019AE
GATE AE 2019 · Paper 1
Aerospace Engineering · Original paper archive
- Section
- Aerospace Engineering
- Question type
- Multiple choice (MCQ)
- Marks
- 2 marks
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