Start Learning CFD Simulation by ANSYS Fluent — Ep 02
Compressible Flow: Steam Ejector
- Lesson
- 02
- Run Time
- 22m 57s
- Published
- May 28, 2026
- Category
- UDF
- Course Progress
- 0%
What You'll Build
This lesson walks you through a CFD simulation of a steam ejector — a mechanical device with no moving parts that uses a primary (motive) steam jet to suck in and mix with a secondary fluid. Ejectors perform two essential jobs: creating vacuum for suction and mixing two fluid streams, and they do it by continuously converting between kinetic and pressure energy as the flow passes through a convergent-divergent nozzle.
In this project, you'll model water vapor as the motive fluid driving the suction of a secondary fluid, watching the flow accelerate beyond the speed of sound and observing how the vacuum-driven suction physically arises.
What You'll Learn
How an ejector works — the physics of vacuum generation, fluid entrainment, and mixing through energy conversion
Why supersonic flow is fundamentally compressible, and how Mach number governs the behavior inside the device
How to design a 2-D convergent-divergent (de Laval) nozzle ejector geometry in Design Modeler
How to generate an efficient structured mesh (~52,000 elements) suited to internal compressible flow
How to set up the density-based solver — the correct choice for compressible and supersonic flows where density varies strongly with pressure
How to handle the pressure difference between primary and secondary inlets that drives the suction phenomenon
How to post-process pressure, velocity, and Mach number contours to trace where the flow goes subsonic, sonic, and supersonic
How to interpret the mixing and compression of the motive and secondary streams downstream of the nozzle throat
Why It Matters
Ejectors are everywhere — refrigeration, vacuum systems, desalination, chemical processing, and power plants. This lesson is your gateway to compressible flow modeling and the density-based solver, skills that carry directly into nozzles, diffusers, supersonic airfoils, and any flow where Mach number matters.