MSc (Hons) and BSc (Hons) in Aerospace Engineering.
Engaged in training forAutomotive CAE Engineer at Fiat Group Automobiles S.p.a. in Pomigliano D’Arco, Napoli, Italy.
Attending Science and Aerospace Technology Ph.D. at Seconda Università degli Studi di Napoli - Aversa, Italy.
Automotive CAE Engineer at Fiat Group Automobiles (FGA) S.P.A. in Pomigliano d’Arco(NA), Italy.
Apr 2012 – present I am asked for modelling and analyse Finite Element Models of both body in white components and full-scale models. The modelling of both steel and plastic components is carried out via HYPERMESH. The stress analysis is the main task I am asked for. Linear analysis, e.g. stiffness of a single part and modal of single parts and full-scale model are performed via NASTRAN (SOL 101,103) while non-linear analysis, also involving the contact modelling, are usually performed via ABAQUS. Implicit and explicit time-dependant simulation using ABAQUS Standard/Explicit. The search for solutions improving the performance in order to match the targets is usually made via FEM using HYPERMESH. Finally, a reporting activity is foreseen.
The chronological order of the activities I have carried out is:
- Door yielding of FIAT Panda using ABAQUS Standard.
- Model of winder mechanism of FIAT 500L using ABAQUS Standard/Explicit.
- Dent analysis of lateral door of FIAT Panda using ABAQUS Standard.
- Dent analysis of trunk lid of FIAT 500L using ABAQUS Standard.
- Member of the team charged of modal development of Jeep 551 (oncoming model) using NASTRAN.
- Member of the team looking for solution about child-head test for Japan approval of Alfa Romeo 4C using LS-DYNA.
- Model of the trunk lid lock mechanism of FIAT 500L using ABAQUS Standard/Explicit.
Trainee at Italian Aerospace Research Centre, Aerothermodynamics Numerical Lab in Capua(CE), Italy.
Jun 2007 – Sep 2007 During the trainee, it has been developed a numerical methodology to investigate hypersonic flow properties by the mean of flow emission spectrum analysis. The work was submitted as my own Bachelor’s Degree Thesis. It has been used the CIRA property CFD code.
MAR 2011 – present Science and Aerospace Technology Ph.D.
Seconda Università degli Studi di Napoli, Naples, Italy.
Research for Aerodynamic Shape Optimization of Winged Re-entry Vehicles.The research activity is about the development of a methodology able to perform a multidisciplinary shape optimization of a reentry vehicle. The main activities concern the design of the geometric model and numerical modelling of the reentry scenario. The routines are usually programmed in C language and APDL (Ansys Design Parametric Language). The optimizations are usually performed via Genetic Algorithm search algorithm.
Master’s Degree in Aerospace Engineeringwith honours
OCT 2007 – DEC 2010 Seconda Università degli Studi di Napoli, Naples, Italy
Thesis: Shape and trajectory optimization of a Winged Re-entry Vehicle.
Bachelor’s Degree Aerospace Engineeringwith honours
OCT 2003 – OCT 2007 Seconda Università degli Studi di Napoli, Naples, Italy
Thesis: Determination of hypersonic flow properties by the analysis of emission spectrum.
Italian – Native language
English – Full professional proficiency
French –Elementary proficiency
Technical skills and competences:
Software: HYPERMESH, ABAQUS, NASTRAN, ANSYS , CATIA V5, ICEM-CFD, CFX, Fluent, Microsoft Office Suite, MATLAB, Tecplot.
Programming Languge:C Language, APDL (Ansys Design Parametric Language), MatLAB, Fortran.
Systems: Windows, Unix.
Viviani A., Iuspa L., Pezzella G., Lanzillo G. (2011). Preliminary Design of Minimum Weight for a ReentryVehicle. CEAS 2011 – 3rd CEAS (Council of European Aerospace Societies) Air & Space Conference, 24-28October 2011, Venice (Italy), Paper ID 0155.
Viviani A., Lanzillo G., Iuspa L. Design of Mass Saving Configuration for Winged Reentry Vehicles. ICAS 2012 – 28th Congress of the International Council of the Aeronautical Sciences,23-28 September 2012, Brisbane (Australia).
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