STRENGTH DETERMINATION AND FAILURE PREDICTION OF COMPOSITE MATERIALS USED IN AIRCRAFT STRUCTURES

Башир Юніс

doi:10.30890/2567-5273.2025-42-01-054

STRENGTH DETERMINATION AND FAILURE PREDICTION OF COMPOSITE MATERIALS USED IN AIRCRAFT STRUCTURES

Автор(и)

Башир Юніс National Aerospace University “Kharkiv Aviation Institute https://orcid.org0000-0002-5693-6954

DOI:

https://doi.org/10.30890/2567-5273.2025-42-01-054

Ключові слова:

composite materials, aircraft structures, strength determination, failure criteria, CFRP

Анотація

Composite materials are extensively used in modern aircraft structures due to their high strength‑to‑weight ratio, excellent fatigue resistance, and corrosion durability. Accurate determination of their mechanical strength is essential to ensure structura

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Опубліковано

2025-12-30

Як цитувати

Юніс, Б. (2025). STRENGTH DETERMINATION AND FAILURE PREDICTION OF COMPOSITE MATERIALS USED IN AIRCRAFT STRUCTURES. Modern Engineering and Innovative Technologies, 1(42-01), 50–60. https://doi.org/10.30890/2567-5273.2025-42-01-054