Machine-translated by Google. Questions are authored in English.
Top

Discussion

Mach Number (Ma) for incompressible flow is :

  • A.Ma > 0.3
  • B.Ma = 0.3
  • C.Ma > 0.4
  • D.Ma < 0.3

Answer: D

Flow is treated as incompressible when Ma < 0.3.

Below a Mach number of about 0.3, the density of a gas changes by only a few per cent as it flows, so it can be treated as incompressible with little error. Above that, compressibility effects become significant and must be included.

Ma = 0.3 is the boundary rather than the region, and Ma > 0.3 or Ma > 0.4 describe flows where compressibility can no longer be ignored.

No comment is present. Be the first to comment.
Loading…

Post your comment

Please log in or register to post a comment.