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Interactional aerodynamic assessment of advanced Tilt Rotor configuration - JTI-CS2-2017-CFP06-FRC-01-15
Deadline: Jun 21, 2017  

 Aerospace Technology
 Aeronautics Industries

Specific Challenge:

The Topic is aimed to investigate, through a modified existing powered wind tunnel model, the fundamental interactional aerodynamic aspects in the tail region of a tilt rotor. The activity will be accomplished by providing a clear understanding of the efficiency (in terms of aircraft static stability) of different empennage configurations when embedded in the rotor inflows. Please refer to the full and formal topic descriptions published in this call.

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