You are doing a problem that requires Reynold's Transport Theorem with Conservation of Mass. You carefully write the equation and then on the second line you write: 0 = V3A3 – ƒvidA1 + fvzdA2 What statements in the question or assumptions you make would lead you to this simplification? Mark all that apply. O The flow is steady. O Newtonian Fluid Incompressible fluid. O Inviscid fluid. Inlets have uniform flow. Exits have uniform flow. O Velocity is only in the x-direction.

Elements Of Electromagnetics
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Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
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You are doing a problem that requires Reynold's Transport Theorem with Conservation of Mass. You
carefully write the equation and then on the second line you write:
0 = v3 A3 - Svị dA1 + f vzdA2
What statements in the question or assumptions you make would lead you to this simplification?
Mark all that apply.
The flow is steady.
Newtonian Fluid
Incompressible fluid.
Inviscid fluid.
Inlets have uniform flow.
Exits have uniform flow.
Velocity is only in the x-direction.
Transcribed Image Text:You are doing a problem that requires Reynold's Transport Theorem with Conservation of Mass. You carefully write the equation and then on the second line you write: 0 = v3 A3 - Svị dA1 + f vzdA2 What statements in the question or assumptions you make would lead you to this simplification? Mark all that apply. The flow is steady. Newtonian Fluid Incompressible fluid. Inviscid fluid. Inlets have uniform flow. Exits have uniform flow. Velocity is only in the x-direction.
Expert Solution
Step 1

Since its a conservation of mass problem, change in intensive property and extensive property is same that is change in mass with respect to time is zero so following cases will arise  

Any mass that doesn't change is control volume is considered to be zero and depending upon the number of closed surfaces, integrals are chosen looking at those closed surfaces.

so the assumptions taken into account is that

  • Density is constant that is it is incompressible.
  • Velocities are constant and not a function of area.

so from above the flow is steady, incompressible fluid, inlets and exit have uniform flow.

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