Juliano Schneiker

Subcontractor (Orizon GmbH). Aeroelastic model development. Maneuver, flight dynamic (gust and turbulence) and dynamic ground loads analysis and flutter analysis. Legacy and Uplift aircraft modifications. (hard point and pod integration).

Main responsibility performing Aeroservoelastic stability analysis and Loads analysis/recovery on the Volocity eVTOL multicopter. Transient multibody analysis coupled with flexible airframe and rotor dynamics, aerodynamics and control using ART Flightlab embedded into in-house tools developed for complete Flight Science usage. Debugging and improvements. Modal basis creation. Static and GVT testing post processing. Modal identification. Linearization of aeroelastic behaviour of rotors

Main responsibility related to the GFEM – Global Finite Element Model of the eVTOL Aircrafts. Superelement creation using CMS techniques to envelop the detailed design into a reduction order model, which is then used for aircraft static, dynamic, landing and flutter evaluations. Model matching against ground vibration testing using modal assurance criteria and optimization techniques. Delivery of global aircraft loads into to the stress teams. Support on MBS, flutter and aeroservoelastic calculations.

Project Engineer at FEV Europe GmbH at the Vehicle and Chassis Integration department and responsible for Fatigue and Damage analysis of Vehicle subcomponents. Dynamic durability calculation of the exhaust line of motorcycles. Implementation of an improved procedure of dynamic stress calculation for frequency response results using FEMFAT Harmonic. Component durability under stochastic loads. Weld durability assessment. Full vehicle dynamic durability calculation under multi axial random loads.

Senior Powertrain FE-Analyses Engineer at MAN Truck and Bus (Euro Engineering AG subcontracted). Powertrain structural FE-Analyses, static non-linear with contact, thermal, modal, and dynamic. Time and frequency domain harmonic and transient dynamic analysis. Static and dynamic stress calculation for fatigue evaluation. Main development of a fatigue calculation procedure for diesel engine crankshafts using harmonic analysis.

Acting as a Senior Powertrain FE-Analyses Engineer Volvo Group Trucks Technology – Powertrain Engineering in Brazil. Powertrain structural non-linear FE-Analyses, modal, static, thermal, contact and dynamic analysis. Time and frequency domain transient dynamic analysis. Static and dynamic stress calculation for thermomechanical fatigue evaluation. 6-month assignment period in Gothenburg / Sweden for further development and of a MBS NVH calculation model for heavy duty engines using AVL Excite PU.

Activities involving the complete Aeroelastic Stability and Response cycle (dynamic + aerodynamic) for the dynamic and aerodynamic FE model development, Flutter calculation and aeroelastic coupling identification, aerodynamic adjustment based on CFD results and Wind tunnel measurements. Aeroservoelastic (aeroelastic + control system) Open Loop and Closed Loop calculations. Development and application of a finite element model optimization methodology used in GVT model adjustments

Thesis: “Jet-wing weight optimization using the aeroelastic criteria”. Structural dynamics, optimization, CAE/FEA, Aeroelasticity

“Numerical and Experimental Analysis of Automotive Mufflers”. Finite Elemente, FORTRAN, Matlab