Andrea Alaimo
Current Organizations / Institutes
The organizations/institutes from the scholar's latest article
Research Subjects
Andrea Alaimo has a total of 26 co-authors. Here are the top co-authors by number of shared publications:
- Calogero Orlando
Department of Engineering and Architecture, Kore University of Enna, 94100 Enna, Italy
22 shared publications - Davide Tumino
Department of Engineering and Architecture, Kore University of Enna, Enna, Italy
12 shared publications - Antonio Esposito
Department of Engineering and Architecture, Kore University of Enna, 94100 Enna, Italy
11 shared publications - Carmelo Rosario Vindigni
Department of Engineering and Architecture, Kore University of Enna, 94100 Enna, Italy
11 shared publications - Giuseppe Mantegna
Department of Engineering and Architecture, Kore University of Enna, Enna, Italy
10 shared publications - Stefano Valvano
School of Engineering and Built Environment, College of Science and Engineering, University of Derby, Derby DE22 3AW, UK
5 shared publications
Latest Publications
- 30 July 2026
- Published by Taylor & Francis in Mechanics of Advanced Materials and Structures
- Vol. 33 (1)
Aeroelastic fragility analysis of wind turbine blades in turbulent flow
1. The prevailing aim in wind turbine design is to develop larger, more powerful systems that extend higher into the atmosphere to capture stronger and more consistent winds; however, increasing th...
- 30 July 2026
- Published by Taylor & Francis in Mechanics of Advanced Materials and Structures
- Vol. 33 (1)
Aeroelastic fragility analysis of wind turbine blades in turbulent flow
1. The prevailing aim in wind turbine design is to develop larger, more powerful systems that extend higher into the atmosphere to capture stronger and more consistent winds; however, increasing th...
- 5 February 2026
- Published by Springer Nature
- p. 48-57
Heat and Mass Transfer in BCC and WBCC Lattice Cores: A Preliminary Study
- 5 February 2026
- Published by Springer Nature
- p. 48-57
Heat and Mass Transfer in BCC and WBCC Lattice Cores: A Preliminary Study
- Open Access
Decision Tree-Based Pilot Workload Prediction Through Optimized HRV Features Selection
This research explores the use of physiological signals derived from heart activity to assess mental effort during flight-related tasks. Data were collected through wearable sensors during simulations with varying cognitive demands. Specific indicators related to heart rate variability (HRV) were extracted and tested in different combinations to identify those most relevant for distinguishing levels of mental workload (WL). A Random Forest (RF) ensemble method is applied to classify two conditions, and its performance is examined under various settings, including model complexity and data partitioning strategies. Results showed that certain feature pairs significantly enhanced classification accuracy. The best features settings obtained from the RF are then used to train the other two decision trees-based classifiers, namely the AdaBoost and the XGBoost. Moreover, the decision trees models output is compared with predictions from a Kriging spatial interpolation technique, showing superior results in terms of reliability and consistency. This study highlights the potential of using heart-based physiological data and advanced classification techniques for developing intelligent support systems in aviation.
Open AccessDecision Tree-Based Pilot Workload Prediction Through Optimized HRV Features Selection
This research explores the use of physiological signals derived from heart activity to assess mental effort during flight-related tasks. Data were collected through wearable sensors during simulations with varying cognitive demands. Specific indicators related to heart rate variability (HRV) were extracted and tested in different combinations to identify those most relevant for distinguishing levels of mental workload (WL). A Random Forest (RF) ensemble method is applied to classify two conditions, and its performance is examined under various settings, including model complexity and data partitioning strategies. Results showed that certain feature pairs significantly enhanced classification accuracy. The best features settings obtained from the RF are then used to train the other two decision trees-based classifiers, namely the AdaBoost and the XGBoost. Moreover, the decision trees models output is compared with predictions from a Kriging spatial interpolation technique, showing superior results in terms of reliability and consistency. This study highlights the potential of using heart-based physiological data and advanced classification techniques for developing intelligent support systems in aviation.
- Open Access
Low-Velocity Impact Behavior of PLA BCC Lattice Structures: Experimental and Numerical Investigation with a Novel Dimensionless Index
Lattice structures are lightweight architected materials particularly suitable for aerospace and automotive applications due to their ability to combine mechanical strength with reduced mass. Among various topologies, Body-Centered Cubic (BCC) lattices are widely employed for their geometric regularity and favorable strength-to-weight ratio. Advances in Additive Manufacturing (AM) have enabled the precise and customizable fabrication of such complex architectures, reducing material waste and increasing design flexibility. This study investigates the low-velocity impact behavior of two polylactic acid (PLA)-based BCC lattice panels differing in strut diameter: BCC1.5 (1.5 mm) and BCC2 (2 mm). Experimental impact tests and finite element simulations were performed to evaluate their energy absorption () capabilities. In addition to conventional global performance indices, a dimensionless parameter, is introduced to quantify the ratio between local plastic indentation and global displacement, allowing for a refined characterization of deformation modes and structural efficiency. Results show that BCC1.5 absorbs more energy than BCC2, despite the latter’s higher stiffness. This suggests that thinner struts enhance energy dissipation under dynamic loading. Despite minor discrepancies, numerical simulations provide accurate estimations of and support the robustness of the index within the examined configuration, highlighting its potential to deformation heterogeneity.Open AccessLow-Velocity Impact Behavior of PLA BCC Lattice Structures: Experimental and Numerical Investigation with a Novel Dimensionless Index
Lattice structures are lightweight architected materials particularly suitable for aerospace and automotive applications due to their ability to combine mechanical strength with reduced mass. Among various topologies, Body-Centered Cubic (BCC) lattices are widely employed for their geometric regularity and favorable strength-to-weight ratio. Advances in Additive Manufacturing (AM) have enabled the precise and customizable fabrication of such complex architectures, reducing material waste and increasing design flexibility. This study investigates the low-velocity impact behavior of two polylactic acid (PLA)-based BCC lattice panels differing in strut diameter: BCC1.5 (1.5 mm) and BCC2 (2 mm). Experimental impact tests and finite element simulations were performed to evaluate their energy absorption () capabilities. In addition to conventional global performance indices, a dimensionless parameter, is introduced to quantify the ratio between local plastic indentation and global displacement, allowing for a refined characterization of deformation modes and structural efficiency. Results show that BCC1.5 absorbs more energy than BCC2, despite the latter’s higher stiffness. This suggests that thinner struts enhance energy dissipation under dynamic loading. Despite minor discrepancies, numerical simulations provide accurate estimations of and support the robustness of the index within the examined configuration, highlighting its potential to deformation heterogeneity. - 18 July 2025
- Published by Springer Nature in International Journal on Interactive Design and Manufacturing (IJIDeM)
- Vol. 20 (4) , 2059-2073
1D Modelling of BCC Lattice Mechanical Behaviour Using Optimised Neural Networks
- 18 July 2025
- Published by Springer Nature in International Journal on Interactive Design and Manufacturing (IJIDeM)
- Vol. 20 (4) , 2059-2073
1D Modelling of BCC Lattice Mechanical Behaviour Using Optimised Neural Networks
- 25 June 2025
- Published by Springer Nature in Acta Mechanica
- p. 1-18
Experimental testing of AlSi10Mg lattice structures manufactured with DMLS technology
- 25 June 2025
- Published by Springer Nature in Acta Mechanica
- p. 1-18
Experimental testing of AlSi10Mg lattice structures manufactured with DMLS technology
- Open Access
- 16 June 2025
- Published by IOS Press
- p. 302-311
A V-Stack Piezoelectric System for Satellites Solar Panels Vibration Damping
In this work a piezoelectric device is proposed for vibration damping on satellites solar panels. The structural arrangement proposed for the piezoelectric actuation system rely on a V configuration of piezoelectric stacks that are hinged to the main yoke structure. The numerical model of the satellite structure is defined in a Euler-Bernoulli beam finite element framework taking into account the electro-mechanical coupling with active elements by introducing their equivalent nodal piezoelectric loads. Different shunt circuits have been designed to suppress the vibrations of the solar panel carrying out a parametric study on the circuit main components parameters to find the best combination. Numerical simulations have been carried out in order to compare the performance of the designed vibration suppression systems proving the effectiveness of the proposed smart structure configuration.
- 16 June 2025
- Published by IOS Press
- p. 302-311
Open AccessA V-Stack Piezoelectric System for Satellites Solar Panels Vibration Damping
In this work a piezoelectric device is proposed for vibration damping on satellites solar panels. The structural arrangement proposed for the piezoelectric actuation system rely on a V configuration of piezoelectric stacks that are hinged to the main yoke structure. The numerical model of the satellite structure is defined in a Euler-Bernoulli beam finite element framework taking into account the electro-mechanical coupling with active elements by introducing their equivalent nodal piezoelectric loads. Different shunt circuits have been designed to suppress the vibrations of the solar panel carrying out a parametric study on the circuit main components parameters to find the best combination. Numerical simulations have been carried out in order to compare the performance of the designed vibration suppression systems proving the effectiveness of the proposed smart structure configuration.
- Open Access
Comparison of Piezoelectric Stack-Based Passive and Active Vibration Suppression Systems for Satellite Solar Panels
This study proposes a piezoelectric device for vibration damping in satellite solar panels. The design features a structural arrangement with piezoelectric stacks configured in a V-shape and hinged to the main yoke structure. The satellite structure is modeled using an Euler–Bernoulli beam finite element framework, incorporating the electro-mechanical coupling of active elements through equivalent nodal piezoelectric loads. Various shunt circuits are designed to mitigate vibrations, with a parametric study conducted to optimize the key circuit parameters. Additionally, a filtered PID active suppression system is developed and tuned using a meta-heuristic algorithm to determine optimal controller gains. Numerical simulations are performed to evaluate and compare the effectiveness of the proposed vibration suppression systems, demonstrating the efficiency of the smart structure configuration and providing performance analysis.
Open AccessComparison of Piezoelectric Stack-Based Passive and Active Vibration Suppression Systems for Satellite Solar Panels
This study proposes a piezoelectric device for vibration damping in satellite solar panels. The design features a structural arrangement with piezoelectric stacks configured in a V-shape and hinged to the main yoke structure. The satellite structure is modeled using an Euler–Bernoulli beam finite element framework, incorporating the electro-mechanical coupling of active elements through equivalent nodal piezoelectric loads. Various shunt circuits are designed to mitigate vibrations, with a parametric study conducted to optimize the key circuit parameters. Additionally, a filtered PID active suppression system is developed and tuned using a meta-heuristic algorithm to determine optimal controller gains. Numerical simulations are performed to evaluate and compare the effectiveness of the proposed vibration suppression systems, demonstrating the efficiency of the smart structure configuration and providing performance analysis.
- 9 February 2025
- Published by Springer Nature
- p. 84-92
A New BCC Lattice Modelling Approach Through a Neural Network Optimisation
- 9 February 2025
- Published by Springer Nature
- p. 84-92
A New BCC Lattice Modelling Approach Through a Neural Network Optimisation
- 7 February 2024
- Published by Springer Nature
- p. 84-92
Additively Manufactured Lattice-Based Structures for Aeronautical Applications
- 7 February 2024
- Published by Springer Nature
- p. 84-92
Additively Manufactured Lattice-Based Structures for Aeronautical Applications