Tesi - Structural Verification Of Dynamic Loads Based On Accelerometric Data
Leonardo Worldwide Corporation
Venegono Superiore, Italy
Not specified; expense reimbursement provided
Hybrid
Master's degree in aerospace or aeronautical engineering
Signal analysis knowledge
Aerospace structural dynamics expertise
The thesis aims to develop a methodology for reconstructing structural stress on aircraft subjected to dynamic loads like aerodynamic buffet using discrete acceleration measurements
Job Summary
The thesis aims to develop a methodology for reconstructing structural stress on aircraft subjected to dynamic loads like aerodynamic buffet using discrete acceleration measurements.
Candidates will analyze flight data, implement a dedicated MATLAB tool, and validate it against unsteady CFD simulations and literature references.
The role offers mentorship from expert tutors, a maximum six-month duration, and expense reimbursement for the student intern.
Matching Summary
The thesis aims to develop a methodology for reconstructing structural stress on aircraft subjected to dynamic loads like aerodynamic buffet using discrete acceleration measurements.
Salary
Not specified; Expense reimbursement provided
Skills & Requirements
Must-have
Master's degree in Aerospace or Aeronautical Engineering
Signal analysis knowledge
Aerospace structural dynamics expertise
MATLAB software proficiency
Nastran Dynamic and Aeroelastic packages
Nice-to-have
Proactive work attitude
Strong team collaboration skills
Learning orientation
Flexibility and communication
English language B2/C1 level
Key Requirements
Laurea Magistrale in Ingegneria Aerospaziale o Aeronautica
Knowledge of Nastran Dynamic and Aeroelastic packages