Salvatore Petrone

• Managed team meetings and discussed project's goals and objectives.
• Defined responsibilities, duties and roles of each team member.
• Numerical and Experimental Aerothermodynamics studies – (ANSYS WB, SPACECLAIM, FLUENT)- CLASSIFIED PROJECT
• CFD Air Intake (FLUENT) - CLASSIFIED PROJECT
• Numerical and Experimental Analysis of electronic assemblies/enclosures and power electronics (ICEPAK) - CLASSIFIED PROJECT
• Numerical and Experimental Structural Analysis of RF mechanical subsystem (ANSYS WB, SPACECLAIM, ICEPAK) - CLASSIFIED PROJECT
• Numerical Bird Strike Analysis (LS-DYNA) - CLASSIFIED PROJECT
• Numerical Aeroelastic Analysis (NASTRAN SOL145 -Flutter, MSC PATRAN/NASTRAN) – CLASSIFIED PROJECT
• Aerothermostructural Analysis of new ceramics Radome (ANSYS WB, SPACECLAIM, FLUENT) - CLASSIFIED PROJECT

• Airbus BELUGA XL FEM Modeling, Superelment of Central Wing Box
• Airbus A400M Redaction of Stress Dossier
• Airbus A350-1000 Certification phase of Hybrid Junction Airbus A350, (NASTRAN SOL 101,105,106); (Hypermesh)
• Airbus A350-1000 Aerodynamics and Aeroelastic Analysis of New Winglet Design of (NASTRAN SOL 144, 145, 146)

• Additive Manufacturing Process Qualification EBM Technologies with ARCAM Q20 printing. Development of method for Topological Optimization and Mechanical Characterization tests (hardness, density, tensile, compression, shear, 3 point bending, fatigue HCF/LCF, fracture toughness KIC e JIC, creep) of specimens in aluminum, steel and titanium. (Materialise Magics, EBM Control, Build Assembler)
• Reduced processing time by analyzing job schedules and implementing appropriate modifications.

• FEM Analysis and Redaction Dossier Calculation CFM Engine Bracket Airbus A320 NEO, Linear & Non Linear Static Analysis of Bracket for the CFM motorization of A320NEO, Modal Frequency Response Analysis (NASTRAN SOL101, 103, 106, 111) of Aft Pylon Fairing for the sonic fatigue calculation.
• DFEM Analysis and Structural Sizing of Bracket Airbus A350-1000, and DFEM Analysis of Pilot Emergency Door in Thermoplastic Composite Material (NASTRAN SOL 101,103, 105,106); (Hypermesh).

Composite DFEM Analysis Airbus A400M, Hand Calculation, Linear& Non Linear Static Analysis, Modal Analysis, and Buckling Analysis (SOL101,103,105,106) with MSC NASTRAN, and MSC PATRAN.

FEM Analysis and Redaction Composite Certification Dossier Airbus A380 for center wing box, centre fuselage A380-800e.

Hand and FEA Calculation fo Keel Beam Airbus A350-900XWB

Linear Static Analysis, Modal Analysis, Buckling Analysis and Non Linear Analysis (SOL101,103,105,106) with MSC NASTRAN, and MSC PATRAN for post-processing phase.