34th Congress of the International Council of the Aeronautical Sciences

02 - Systems Engineering and Integration

AUTOMATION OF ENGINEERING INTEROPERABILITY FOR AIRCRAFT SYSTEM DESIGN

F. During¹, R.C. Munjulury¹, R. Hällqvist, System Simulation and Concept Development, Saab Aeronautics, Sweden; ¹FLUMES, Linköping University, Sweden

The work showed that an automated framework can estimate the pressure loss coefficient for an internal flow system with good accuracy as well as merge the CAD model with other topological simulation models. By automatically updating the pressure loss coefficients when re-designing a flow system, a simulation can be run whit pre-packaged parameters reducing the risk for errors.


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