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[HTML][HTML] Multiaxial loading of aeronautic composite structures at intermediate scale: A review of VERTEX developments
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 …
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 …
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 …
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 …
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 …
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 …
предложена общая методика (алгоритм) определения минимальных толщин при …