For supersonic compression flows, there is a bow shock formed at the – McqOptions

MCQOPTIONS

1.	For supersonic compression flows, there is a bow shock formed at the mouth of the Pitot tube.
A.	False
B.	True
Answer» C.

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Related MCQs

The Rayleigh Pitot tube formula does not relate which of these quantities to the others?
For supersonic compression flows, there is a bow shock formed at the mouth of the Pitot tube.
For subsonic compressible flow, which of these is not required to be measured separately to find the velocity of flow?
For compressible flow also, we can calculate velocity with the Pitot and static pressure found.
The definition of stagnation pressure can help us calculate the velocity of sound for an incompressible flow. What else do we need for the calculation?