Aniello Riccio

Professor

Università degli Studi della Campania Luigi Vanvitelli

Italy

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Professor Aniello Riccio is a faculty member at the Università degli Studi della Campania Luigi Vanvitelli in Italy. His research focuses on advanced materials and structural design, particularly in the context of aerospace engineering. His recent work includes innovative approaches to UAV structures, composite panels, and aerodynamics using shape memory alloys and lattice designs.

Aniello Riccio

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Articles (21)

Redesigning UAV Vertical Tail Structures with Lightweight Eco-Friendly Carbon-Reinforced Polymers: A Generative Design-Based Approach

Mimicking Alveolar Lung Structures with Lattice Designs

A Numerical Investigation on the Influence of Geometric Curvature on Delamination Growth in Curved Stiffened Composite Panels

Influence of Electrical Parameters in a Composite Wing Actuated by Shape Memory Alloys Wires: A Numerical–Experimental Study

An Experimental Approach for Investigating Fatigue-Induced Debonding Propagation in Composite Stiffened Panels Using Thermographic Phase Mapping

Morphing Spoiler for Adaptive Aerodynamics by Shape Memory Alloys

A systematic review of design for additive manufacturing of aerospace lattice structures: Current trends and future directions

Optimization of composite aeronautical components by Re-designing with double-double laminates

Non-Conventional Wing Structure Design with Lattice Infilled through Design for Additive Manufacturing

Unstable Delamination Growth in Stiffened Composite Panels Under Cyclic Loading Conditions

On the effectiveness of double-double design on crashworthiness of fuselage barrel

Shape Memory Alloys Applied to Automotive Adaptive Aerodynamics

Experimental investigation on 3D printed lightweight sandwich structures for energy absorption aerospace applications

Delamination Effect on the Buckling Behaviour of Carbon–Epoxy Composite Typical Aeronautical Panels

A Numerical Study on Carbon-Fiber-Reinforced Composite Cylindrical Skirts for Solid Propeller Rockets

Numerical-experimental study on the compressive behaviour of repaired composite panels

Experimental and numerical assessment of the impact behaviour of a composite sandwich panel with a polymeric honeycomb core

Fatigue driven delamination in composite structures: Definition and assessment of a novel fracture mechanics based computational tool

Influence of Delamination Size and Depth on the Compression Fatigue Behaviour of a Stiffened Aerospace Composite Panel

On the Crashworthiness Behaviour of Innovative Sandwich Shock Absorbers

A Feasibility Study on Innovative Reinforced Modular Frames for Automotive Applications

Collaborators (2)

Alfonso Reginelli

Michele Visone

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