A method for loading the structurally similar sample of a thick-walled composite three-span stringer panel of the wing torsion box by combined action of the compressive and shear loads
Published: 08.09.2025
Authors: Perelomov K.A.
Published in issue: #9(165)/2025
DOI: 10.18698/2308-6033-2025-9-2474
Category: Aviation and Rocket-Space Engineering | Chapter: Design, Construction, Production, Testing, and Operation of Aircraft