Features of fatigue and damage-tolerance tests of full-scale metal-composite aircraft structures
Author:
Affiliation:
1. Central Aerohydrodynamic Institute (TsAGI)
Publisher
TEST-ZL Publishing
Subject
Condensed Matter Physics
Reference16 articles.
1. Strizius V. E. Mechanisms of accumulation of fatigue damage under complex program loading of layered composites: existing hypotheses / Nauch.-Tekhn. Byull. SPbPU. Estestv. Inzh. Nauki. 2019. Vol.25. N 4. P. 71 – 82 [in Russian]. DOI:10.18721/JEST.25406
2. Brunner A. J. Scatter, Scope and Structures: What fatigue fracture testing / 39th Risø International Symposium on Materials Science / IOP Conf. Series: Materials Science and Engineering 388 012003. 2018. — 19 p. DOI:10.1088/1757-899X/388/1/012003
3. Ushakov A. E. Methodology for ensuring operational survivability and safety of aircraft structures from PCM. — Moscow: Fizmatlit, 2012. — 203 p. [in Russian].
4. Quaresimin M., Zappalorto M., Maragoni L. A damage-based modelling framework for the fatigue damage evolution in composite laminates / Semantic scholar / Mater. Sci. 2018. P. 1456 – 1462. DOI:10.1063/1.5045901
5. John E. McCarty. Full-Scale Structural Testing / Composites. Vol.21: ASM Handbook / ASM International. 2001. P. 794 – 799. DOI:10.31399/asm.hb.v21.a0003445
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