Heated Laminar Pipe (Constant Wall Heat Flux)

verification

Developing temperature field
Temperature on a streamwise plane through the pipe axis: the uniform inlet temperature rises along the heated wall as the thermal boundary layer grows and the bulk temperature climbs nearly linearly downstream.

Overview

This case verifies the solver's convective heat-transfer prediction for the textbook problem of fully-developed laminar flow in a circular pipe with a uniform wall heat flux. When both the velocity and temperature fields are fully developed, the Nusselt number reaches the exact analytic value Nu=hD/k=48/11=4.3636, a constant that is independent of the Reynolds number Re and Prandtl number Pr. Reproducing this dimensionless number, and the way the local Nusselt number decays from the thermal entrance toward it, exercises the coupled momentum and energy solution for an incompressible, constant-property fluid.

Problem Setup

The geometry and flow are those of the companion Hagen–Poiseuille case: a straight circular pipe of diameter D=0.2 m and length L=20 m, with a uniform inlet velocity giving Re=ρVD/μ=500. The fluid is incompressible (constant density) with the energy equation active, a Prandtl number Pr=0.7, and constant properties. The wall is a no-slip boundary carrying a uniform heat flux into the fluid; the inlet temperature is uniform and the outlet is a static-pressure boundary.

With Re=500 and Pr=0.7 the thermal entrance length is 0.05RePrD3.5 m, so the flow is both hydrodynamically and thermally fully developed over the downstream portion of the pipe, where the Nusselt number is sampled.

Quantities of Interest

The primary quantity is the Nusselt number Nu=hD/k, where the convective coefficient h=q/(TwTb) is formed from the imposed wall heat flux q, the local wall temperature Tw(x), and the mass-flux-weighted bulk (mixing-cup) temperature Tb(x)=uTdA/udA across the cross-section. The local Nu(x) is high in the thermal entrance region and relaxes onto the fully-developed plateau; the developed-region value, averaged over 15x19 m on the finest grid, is Nu=4.3783, within 0.34% of the exact Nu=48/11=4.3636.

Sources

T. L. Bergman, A. S. Lavine, F. P. Incropera, D. P. DeWitt, Fundamentals of Heat and Mass Transfer, 7th ed., Wiley, 2011.: https://books.google.com/books/about/Fundamentals_of_Heat_and_Mass_Transfer_7.html?id=5cgbAAAAQBAJ
Fully-developed laminar pipe flow with uniform wall heat flux: Nu=48/11=4.36, independent of Re and Pr.
F. M. White, Viscous Fluid Flow, 2nd ed., McGraw-Hill, 1991.: https://openlibrary.org/books/OL1878619M/Viscous_fluid_flow
Constant-heat-flux Nusselt number for fully-developed laminar pipe flow.

Results

Local Nusselt number Nu(x)

Local Nusselt number \( Nu(x) \)
Local Nusselt number along the pipe (finest grid). Nu(x) decays from the high values of the thermal entrance region and settles onto the fully-developed constant-flux value Nu=48/11=4.36.

Reference: T. L. Bergman, A. S. Lavine, F. P. Incropera, D. P. DeWitt, Fundamentals of Heat and Mass Transfer, 7th ed., Wiley, 2011. (Nu=48/11=4.3636 (uniform wall heat flux)): https://books.google.com/books/about/Fundamentals_of_Heat_and_Mass_Transfer_7.html?id=5cgbAAAAQBAJ

Fully-developed Nusselt number vs 48/11

SourceNu
Luminary 4.3783
Fully developed (48/11) 4.3636

Nusselt number averaged over the fully-developed region (15x19 m) on the finest grid, compared with the exact constant-heat-flux value Nu=48/11=4.3636.

Solver configuration

features exercised
Verification3DLaminarConstant densitySteadyEnergy equation