Evaluation of the Suitability of the Strain-Gauge Method for Measuring Deformations during the Fatigue Tests of Aviation Composite Structures

Publicado en línea: 09 ago 2018

Páginas: 75 - 84

DOI: https://doi.org/10.1515/fas-2017-0006

Palabras clave

aviation composite structures, fatigue tests, strain-gauge method, deformation measurements

© 2017 Marek Rośkowicz et al., published by Sciendo

This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 3.0 License.