The reduction of stress concentrations in adhesive joints with the use of curved aluminum adherends
VDC Pires, FCC Ribeiro, RJC Carbas… - Mechanics of …, 2023 - Taylor & Francis
The study proposes a novel concept of a curved single lap joint (SLJ) with non-uniform
adhesive thickness to reduce stress concentrations near overlap edges. Experimental and …
adhesive thickness to reduce stress concentrations near overlap edges. Experimental and …
Delamination prevention of composite joints with asymmetric carbon-fiber reinforced plastic adherends
VDC Pires, RJC Carbas… - Journal of …, 2024 - journals.sagepub.com
The use of adhesive bonding in aeronautical applications has gained popularity due to its
numerous advantages over traditional mechanical fastening methods. However, the issue of …
numerous advantages over traditional mechanical fastening methods. However, the issue of …
Experimental analysis of tensile strength of 6-layer carbon/kevlar/epoxy hybrid composite reinforced with nano-graphene/silica nanoparticles
I Voghofi, F Ashenai Ghasemi… - … of Elastomers & …, 2024 - journals.sagepub.com
The main aim of the present research is to improve the static tensile strength of
Carbon/Kevlar/Epoxy hybrid composite by adding different nanoparticles. To this end, two …
Carbon/Kevlar/Epoxy hybrid composite by adding different nanoparticles. To this end, two …
An analytical solution to “pillowing effect” for composite fuselages
J Feng, C Li, Z Xiao - Journal of Physics: Conference Series, 2024 - iopscience.iop.org
Abstract" Pillowing effect", introduced by inner cabin air pressure on stringer-frame stiffened
fuselage cylinder, is a critical loading case for civil aircraft fuselage. The" pillowing effect" …
fuselage cylinder, is a critical loading case for civil aircraft fuselage. The" pillowing effect" …