Difficulty: Easy
Correct Answer: 4/3
Explanation:
Introduction / Context:The momentum correction factor β accounts for the non-uniform velocity profile when converting between average-velocity-based momentum flux and the actual momentum flux. It is essential in accurate force and thrust computations for ducts and nozzles.
Given Data / Assumptions:
Concept / Approach:
Definition: β = (∫_A ρ u^2 dA) / (ρ A u_avg^2). For a parabolic profile u(r) = u_max * (1 − (r/R)^2), the integrals can be evaluated analytically to obtain a constant β for laminar flow in a circular pipe.
Step-by-Step Solution:
Compute u_avg = (1/A) ∫_A u dA = u_max/2.Compute ∫_A u^2 dA using polar area element 2π r dr and the parabolic u(r).After integration, β = (∫ u^2 dA) / (A u_avg^2) = 4/3 ≈ 1.333.Verification / Alternative check:
Known standard results: energy correction factor α = 2 (laminar pipe), momentum correction factor β = 4/3. For turbulent flow, both factors are closer to 1 due to flatter profiles.
Why Other Options Are Wrong:
1/2, 2/3, 3/4, 3/2 do not match the parabolic-profile integration result for laminar pipe flow.
Common Pitfalls:
Confusing α (energy correction) with β (momentum correction), or using turbulent values (near 1) for laminar cases.
Final Answer:
4/3
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