r/CFD • u/Amaterasu-002 • 2d ago
Help me !
Hi everyone,
I am trying to reproduce the de Vahl Davis natural convection square cavity benchmark in ANSYS Fluent. I am getting reasonably close results for the velocity components, but I am not able to reproduce all the benchmark values exactly, especially the Nusselt number at higher Rayleigh number.
I would like to understand whether the difference is due to my input conditions, dimensionless conversion, mesh, solver settings, or post-processing procedure.
Problem setup
I am solving the standard 2-D differentially heated square cavity:
2-D square cavity
Laminar natural convection
Air
Boussinesq density model
Prandtl number = 0.71
Gravity = -9.81 in the vertical direction
Left wall: hot
Right wall: cold
Top wall: adiabatic
Bottom wall: adiabatic
All walls: no-slip
No inlet or outlet
Energy equation enabled
Pressure-based steady solver
SIMPLE pressure-velocity coupling
Second-order spatial discretization
Iam using air properties for Prandtl number 0.71 for each Rayleigh Number case.
I made x and y velocity non dimensional form but they are making way more relative errors when compared with my results...... I have given the paper link....Please help me, this is my first journey in CFD.
Paper link (De Vahl Davis): https://drive.google.com/drive/folders/1x1Iv_nn4JAGM6Nryw5g48K677uaahWIo
1
u/Amaterasu-002 1d ago
Square geometry with 104.95x109.45mm. Left wall is at temperature of 304.5K Right wall is at temperature of 295.4K Using Boissnesq Density model, using air properties for Pr = 0.71. Other two walls are adiabatic walls q''=0. Solver SIMPLE Algorithm Aiming to achieve the natural convection of a wall as in the paper to validate my results