CS-002: MID-AIR REFUELING OF A MIRAGE F1 FIGHTER
This case study describes how Aerosud employed Flownex to model flow rates and refueling sequences in the modified refueling system for the re-engined Mirage F1 Fighter, while also analyzing valve failure scenarios to ensure system safety during single-point failures.
Share This:
Share This:
More Case Studies
You might also be interested in these CASE STUDIES
CS-069: Investigating a Delay in O2 Response in an Air/Fuel Gas System
This case study investigates a delay in airflow response during transient load changes in a fossil fuel power station, where Flownex SE identified that optimizing feedforward control and
CS-068: Energy and Exergy in a Brayton Cycle-Based Power Conversion Unit
This case study simulated a Brayton cycle PCU in Flownex SE under steady-state conditions, logging parameters to calculate energy and exergy, and testing fault conditions by adjusting component
CS-067: Design of Low Temperature Proton Exchange Membrane Fuel Cell System Components
This case study demonstrates the use of Flownex to model system components of a low-temperature proton-exchange membrane fuel cell (PEMFC), including the cathode-side air flow…
CS-066: Data Centre Free Cooling Analysis Using Flownex SE
This case study demonstrates how Flownex SE simulates free cooling in a data center using natural resources and weather data in a transient analysis to optimize…
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