Gallery

DFTS

Fluid-Structure-Interaction in the ditch tool – November 2016

Development of benchmark geometries - January 2017

Coupling of CFD and FEM

Two-phase flow simulation of aircraft ditching

SPH Simulation of a rigid Airbus CN 235 at model scale

EADS-CASA CN235-300M Model for scaled-model ditching test

Generic helicopter with inflated floatation device

Partial structure test modelled with Ditcher

This project has received funding from the European Union’s Horizon 2020 research and innovation programme under grant agreement No 724139.

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