Abstract

International audience; The reduced code linearity test technique for pipeline ADCs consists in measuring some judiciously selected codes which contain the information about the linearity of the converter as opposed to the standard histogram technique that considers indiscriminately [...]

Abstract

 

Carbon fibre reinforced polymer composite material structures continue to be, despite the tremendous technological maturity achieved in recent decades, one of the most promising options to address the challenges of the aeronautical industry with respect to behaviour [...]

Abstract

This paper describes the Fatigue & Damage Tolerance Phase for the S19.1 Full Component Test of the A350 XWB Aircraft.   The aim of this test was to demonstrate that the fatigue phenomena does not occurs, as well as no crack growing on composite materials. A350XWB [...]