Design-theoretical and experimental determination of physical and mechanical properties of the composite materials for the light aircraft fuselage multilayer load-bearing elements
Published: 03.10.2024
Authors: Tun Lin Htet, Prosuntsov P.V.
Published in issue: #10(154)/2024
DOI: 10.18698/2308-6033-2024-10-2392
Category: Aviation and Rocket-Space Engineering | Chapter: Strength and Thermal Conditions of Aircraft