CS-084: REGENERATIVE BURNER
This case study shows how Flownex was used to model a regenerative burner and quantify its waste-heat-recovery efficiency.
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CS-065: Validating a Scaling Procedure for Cryogenic Pressure Fluctuations
This case study illustrates how Flownex was used with a scaling procedure based on dimensional analysis to simulate transient pressure fluctuations in a scaled cryogenic fluid flow system,
CS-064: Design of a Mobile Liquid Rocket Engine Test Facility Fuel Feed System using Flownex
This case study highlights how Flownex was used to model the propellant feed system for the SAFFIRE rocket engine, determining tank pressure and flow characteristics, with results validated
CS-063: Modelling of Spacecraft Propulsion System Priming in Flownex
This case study shows how Flownex was used as a tool to model a fuel feed system’s priming procedure, recording dynamic pressures during a transient simulation and investigating
CS-062: Lightweight Pressure Regulator for Space Launch Vehicles
This case study focuses on the design of a regulator for a suborbital launch vehicle developed by the Aerospace Systems Research Institute, utilizing Flownex to simulate and ensure
CS-061: GAS TURBINE COMBUSTOR DESIGN
This case study demonstrates how Flownex was used to model three combustor types—two annular and one reverse flow—showing its effectiveness in handling complex geometries, avoiding numerical issues, and
CS-060: ROCKET ENGINE FEED CYCLES AND COOLING TECHNIQUES IN FLOWNEX
This case study details the investigation conducted by UKZN’s Aerospace Research Institute into the development of a Commercial Launch Vehicle (CLV) for South Africa, utilizing Flownex to model
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