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 various propellant feed cycles and cooling techniques in order to enhance rocket engine performance and optimize payload capacity for satellite launches.
Share This:
Share This:
More Case Studies
You might also be interested in these CASE STUDIES
CS-083_Dynamic Modelling of a Sodium-Cooled Fast Reactor During a Loss-of-Flow Event
This case study describes how Flownex was used to model axial turbines stage-by-stage using a nozzle-based approach that reproduces turbine behavior accurately even when limited geometric data is
CS-089: Simulating Tailings Transfer Upgrades
This case study describes how Flownex was used to model axial turbines stage-by-stage using a nozzle-based approach that reproduces turbine behavior accurately even when limited geometric data is
CS-082: Accurate Stage by Stage Axial Turbine Modelling with Minimal Geometry
This case study describes how Flownex was used to model axial turbines stage-by-stage using a nozzle-based approach that reproduces turbine behavior accurately even when limited geometric data is
CS-080:Predicting Combustor Wall Temperatures Using Thermal Fluid Network Modelling
This case study shows how Flownex thermal-fluid network model was used to predict the temperature distribution along the conical bluff body of an academic combustor. The model is
CS-081: Exhaust Gas Recirculation on Gas-Turbine Engine
This case study shows how Flownex was used to evaluate and optimize condensate extraction pump (CEP) flow control at a 4100 MW coal-fired power station. The plant originally
CS-078: Emergency Vent Flare Ice Build-Up Estimation
This case study shows how Flownex was used to evaluate and optimize condensate extraction pump (CEP) flow control at a 4100 MW coal-fired power station. The plant originally
