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What is the orientation of a normal shock with respect to the upstream fluid flow?
Fluid flow changes from _________ to ___________ across a normal shock.
What happens to the static flow properties (pressure, density, temperature) across any shock wave?
Mach angle is defined as:
What is the condition for the formation of detached shock wave?
When does an oblique shock form in a supersonic flow?
For a normal shock, which of the following is true according to the Prandtl (or Meyer) relationship?
When does an expansion wave form in a supersonic flow?
The flow across an expansion fan is assumed as:
Total pressure across an expansion fan _________ and across a shock wave __________.
Flow Mach number across an expansion wave ____________
For the same supersonic flow conditions, the oblique shock wave angle for a 2D wedge is ________ a 3D cone.