[HTML][HTML] Multiaxial loading of aeronautic composite structures at intermediate scale: A review of VERTEX developments

B Castanié, JC Passieux, JN Périé, C Bouvet… - Composites Part C …, 2024 - Elsevier
The certification of aeronautical composite structures is based on a pragmatic approach,
which is intended to be safe and essentially experimental but with a strong test/calculation …

MULTIAXIAL TESTING OF AERONAUTIC COMPOSITE STRUCTURES 1 MULTIAXIAL TESTING OF AERONAUTIC COMPOSITE STRUCTURES AT INTERMEDIATE …

B Castanié, JC Passieux, JN Périé… - … -34th Congress of …, 2024 - insa-toulouse.hal.science
The certification of aeronautical composite structures is based on a pragmatic approach,
which is intended to be safe and essentially experimental but with a strong test/calculation …

[PDF][PDF] MULTIAXIAL TESTING OF AERONAUTIC COMPOSITE STRUCTURES AT INTERMEDIATE SCALE

JS Dufour - icas.org
The certification of aeronautical composite structures is based on a pragmatic approach,
which is intended to be safe and essentially experimental but with a strong test/calculation …

The Wing Caisson Orthotropic Panels Thicknesses Determining at the Supercritical State with Regard to Membrane and Bending Stresses

M OV, EY Toropylina - vestnikmai.ru
The skin buckling is allowed for the upper load-bearing panels of the small and medium
weight-lift ability aircraft caisson at the load exceeding operational level. The authors noted …

Определение толщин ортотропных панелей кессона крыла при закритическом состоянии с учётом мембранных и изгибных напряжений

ОВ Митрофанов, ЕЮ Торопылина - vestnikmai.ru
Аннотация Для композитных панелей с учетом допустимого закритического поведения
предложена общая методика (алгоритм) определения минимальных толщин при …