NAFEMS Rupture Test of an Airbus Vertical Tail CFRP Fitting: Design of Loading and Tracking of Test Results by Non Linear FEA

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Rupture Test of an Airbus Vertical Tail CFRP Fitting: Design of Loading and Tracking of Test Results by Non Linear FEA

This paper was presented at the 2009 NAFEMS World Congress held in Crete, Greece.

Document Details

Reference	NWC09_8
Author	Barthold. U
Language	English
Type	Paper
Date	16th June 2009
Organisation	CADFEM

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Rupture Test of an Airbus Vertical Tail CFRP Fitting: Design of Loading and Tracking of Test Results by Non Linear FEA

Document Details

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