Compressible flow · evidence summary

A longer run still fails the physics checks.

A difficult compressible-flow setup can tempt a team to invest in larger meshes before isolating the actual failure.

The research prompt

Original research prompt

use openfoam to do a RANS turbulence modeling of supersonic gas eductor

A diagnosis, with performance unresolved.

The staged CFD case reached 410,400 cells, but mass imbalance remained around 50%. The useful output was the failure diagnosis and a proposed next solver test.

No accepted entrainment ratio. A transient-solver alternative was proposed but not run successfully in this record.

The recorded investigation

Build the OpenFOAM setup

The record develops a specialist and a steady compressible RANS case with a k–ω SST turbulence model.

Challenge the mesh explanation

A 51,300-cell coarse case also fails, weakening the claim that fine-grid geometry alone explains the problem. The proposed very large remesh was not executed.

Improve numerical survival without accepting the answer

After revised turbulence initialization, one reported run reaches about 1,150 iterations but still fails. Residuals and mass balance remain unacceptable.

Preserve the diagnosis and next proposal

The final staged case has 410,400 cells. A transient solver and inlet-boundary revision are proposed next, not demonstrated as successful.

Where the conclusion stops

The next useful test

Review the boundary conditions, then authorize and validate a bounded transient test with explicit convergence and mass-balance acceptance criteria.

Selected scientific files

These files support inspection of the study. They are not a complete package of run inputs, dependencies or raw outputs. Scientific scripts are provided for reading; this website does not execute them.

This is an editorial evidence summary of a recorded investigation, including later requests and review. The prompt animation is a presentation of saved work, not a live simulation. Human time saved was not measured.