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Thermo-Mechanical Virtualization of Hybrid Flax/Carbon Fiber Composite for Spacecraft Structures

Projekter: Projekt › Forskning

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Beskrivelse

The goal of this project is to develop a thermomechanical hybrid simulation setup for testing composite component for aerospace applications.
Kort titelThermo-Mechanical Virtualization of Hybrid Flax/Carbon Fiber Composite for Spacecraft Structures
AkronymTHERMICS
StatusAfsluttet
Effektiv start/slut dato01/11/2016 → 31/01/2018

ID: 194483696