Quantitative method in assessing the integrity level of composite structures in the helicopter airframe units depending on their design parameters
Authors: Kisin I.D., Zavalov O.A.
Published in issue: #2(158)/2025
DOI: 10.18698/2308-6033-2025-2-2425
Category: Aviation and Rocket-Space Engineering | Chapter: Design, Construction, Production, Testing, and Operation of Aircraft