Difficulty: Easy
Correct Answer: 5 × 10^5
Explanation:
Introduction:Reynolds number is a dimensionless ratio that compares inertial to viscous forces in a fluid flow. For external flow over a flat plate, it is common to characterize transition from laminar to turbulent boundary layers using a critical local Reynolds number, Re_x, based on distance from the leading edge. Knowing the approximate threshold for turbulence helps in estimating skin friction, heat transfer, and mass transfer rates in engineering design.
Given Data / Assumptions:
Concept / Approach:Experiments show that on a smooth, nominally two-dimensional flat plate with low free-stream turbulence, transition commonly begins when Re_x is of the order of 3 × 10^5 to 10^6. A widely used design value is about 5 × 10^5. Above this threshold, small disturbances amplify, causing the laminar boundary layer to transition to turbulent, which increases skin friction and heat transfer coefficients but also enhances mixing near the wall.
Step-by-Step Solution:
1) Identify the parameter controlling transition: Re_x = (rho * U * x) / mu.2) Recognize canonical threshold used in textbooks and design correlations: about 5 × 10^5.3) Compare options and select the closest standard critical value.4) Conclude that Re_x greater than 5 × 10^5 generally indicates turbulent boundary layer onset.5) Note that higher free-stream turbulence or surface roughness can shift transition earlier (lower Re_x).Verification / Alternative check:Flat-plate correlations for friction factor and Nusselt number often piecewise combine laminar and turbulent formulas with transition near Re_x ≈ 5 × 10^5. Wind tunnel and water channel measurements support this conventional benchmark under low-disturbance conditions.
Why Other Options Are Wrong:
Common Pitfalls:Assuming a single universal critical value regardless of surface finish, pressure gradient, or free-stream turbulence. Transition is sensitive; use 5 × 10^5 as a design reference but validate for specific environments.
Final Answer:5 × 10^5
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