WerkenbijnlrAerospace Vehicles

Master thesis assignment: Tilt-rotor-wing aerodynamic modelling for aeroelastic analysis

Amsterdamhybrid

Posted 5 days ago · via Recruitee

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About this role

What will you be doing? Tilt-rotor aircraft offer a significant advantage over conventional helicopters in terms of cruise speed and efficiency. NLR is currently preparing a wind tunnel test of a tilt-rotor-wing configuration. The focus of the wind tunnel test is aeroelastic stability (i.e. flutter and limit-cycle oscillations). The goal of this test is to gather data for validation of comprehensive analysis tools. To assist the aeroelastic wind tunnel model design & development, simulations with a comprehensive rotorcraft modelling software are performed as well. The comprehensive modelling software that is used for these investigations offers various methods to model the aerodynamics of the tilt-rotor-wing model.…

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