Shanghai
China
Donghua University - Center for Civil Aviation Composites
Hybrid effect, hybrid ratios, hybrid laminated composite, ballistic impact damage, finite element analysis.
Additive manufacturing, capillary-driven 3D printing, continuous fiber composite, free space printing, thermosetting resin
3D braided carbon fiber/epoxy composites, thermal strain, coefficient of thermal expansion (CTE), cooling rate
Solar interfacial evaporation, Hydrogel, Cellulose nanofibers, desalination, Anti-pollution
3D angle-interlock woven composites, thermo-oxidative aging, damage mechanics, deep learning
A, Thermosetting composites B, Hot diaphragm preforming C, Defect D, Fiber deflection
3-D braided composites, Braided structures, Mode-I fracture, Low-velocity impact (LVI), Finite element analysis (FEA)
Carbon fiber reinforced polymer, Continuous-wave laser irradiation, Laser-Induced Damage, Residual tensile strength, Laser ablation, Heat-affected zone.