Dipl.-Ing. Leandro Bergamo M.Sc.

Embraer Defense and Security: Flight mechanics analysis, modeling and simulation, specification of flight test proposal and weapon integration of several programs at Embraer Defense and Security. Development of Simulink models and Matlab tools for flying qualities analysis.

JAS-39 Gripen E/F: Transfer of technology project for the Brazilian Air Force F-39 program.

Embraer 190E2/195E2 program: Flight mechanics analysis, modeling and simulation, flying qualities requirements specification of fly-by-wire aircraft, specification of flight test proposal. Development of Simulink models and Matlab tools for flying qualities analysis and requirements verification. Embraer 190 fleet analytics: Development of neural network models for mass and balance estimation using post-flight fleet data.

Super Petrel LS: LSA aircraft certification, structural analysis, aerodynamic analysis and design, flight test, quality assurance.

This master thesis analyzed hydrodynamic instability of the subsonic compressible flow inside a lid-driven cavity. A high fidelity DNS solver with parallel computation capability was implemented to generate basic flows. The BiGlobal approach was used to study the hydrodinamic instability. The effect of Mach number on critical Reynolds number was obtained (neutral curves for several Mach numbers). New intrinsically compressible modes were found.

2005: Member of SAE Aerodesign team. - Aerodynamics - Flight performance - Flight dynamics 2009-2010: Scientific initiation. - Computational Simulation of Noise Generated by Flow via DNS and Acoustic Analogy