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Fully developed circular-pipe model

Round-Duct Straight-Run Pressure Loss

Calculate distributed wall-friction loss for a straight constant-diameter circular duct with supplied fluid density, viscosity and absolute roughness. Transitional flow and unmodelled fittings are not guessed.

Darcy factorLaminar/ColebrookStraight run only

Cakupan: distributed friction in a fully developed straight circular run only. Add entrances, exits, bends, dampers, transitions, branches and other local losses separately from sourced K values. Do not use this incompressible model when density changes materially along the run.

Straight-run result

Pressure drop ΔP
Pressure gradient
Mean velocity v
Bilangan Reynolds
Darcy friction factor f
Rezim

A=πD²/4;   v=(Q/3600)/A;   Re=ρvD/μ
ΔP=f(L/D)ρv²/2;   f=64/Re for Re<2300
1/√f=−2log₁₀[ε/(3.7D)+2.51/(Re√f)] for Re≥4000

Sebuah NREL/US DOE HVAC modelling presentation documents Darcy-Weisbach with laminar and turbulent friction-factor treatment. NASA defines Re=ρvL/μ as the inertial-to-viscous similarity parameter.

A NASA pipe-flow reference places transition usually between Re 2300 and 4000 depending on disturbances. No single regime equation is asserted in that interval, so this calculator reports it as out of scope. The DOE fluid-flow handbook notes viscosity is a fluid property affected by temperature.

Removed claims: the former page hard-coded ρ=1.2 kg/m³ and μ=1.81×10⁻⁵ Pa·s without conditions, called a Haaland explicit approximation “Colebrook”, and applied it immediately above Re 2300. Unsourced roughness/velocity/equivalent-length presets and rectangular-duct shortcut were removed.

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Straight circular-run friction only; verify fluid properties and local losses. Scientific review: July 2026.

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