Frequently Asked Question

Transition is the change from orderly laminar motion to turbulent motion. It depends on Reynolds number, pressure gradient, surface roughness, free-stream disturbances, curvature, and wall heating or cooling.

A single critical Reynolds number is not universal. Treat transition location as a model-sensitive output unless the inflow disturbance environment and surface condition are well characterized.

Closure and scale awareness

Turbulent flow contains fluctuating velocity and pressure over a range of interacting scales. Averaging introduces additional correlations, such as turbulent momentum transport, that are not determined by the mean variables alone. A closure model is therefore an assumption about how unresolved transport relates to resolved gradients or other modeled quantities. Its suitability depends on Reynolds number, wall treatment, separation, curvature, buoyancy, compressibility, and the engineering output.

U is mean velocity and u′ is a fluctuation. The turbulent stress is not a universal constant; it depends on the flow and the adopted closure.

Worked example

For a duct with D_h = 0.10 m, U = 20 m/s, ρ = 1.2 kg/m³, and μ = 1.8×10⁻⁵ Pa·s, Re = ρUD_h/μ = 133,000. A laminar assumption then needs strong physical justification. Compare pressure loss, wall behavior, and sensitivity to near-wall resolution before accepting a model.

Limit: residual reduction alone cannot establish turbulence-model adequacy.

Engineering check

For Laminar–Turbulent Transition, maintain traceability from requirement to risk, design output, evidence, and approval. Record the configuration, acceptance criterion, test or analysis conditions, open actions, and residual risk. A method is not complete when the document is filled in; it is complete when the evidence supports the decision and affected controls are updated.