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ONERA-ISA

ONERA-ISA


Transfert de technologie

Aero-Acoustic/Performance Optimisation of 3D Propellers and Rotors

Applications

Active Blade Rotor
 
Airplane Propeller

 > Aeronautics

  • Design of optimised aircraft propellers and rotors- noise reduction/performance.

Keywords

  • Noise reduction, Performance, Multidisciplinary optimisation, Rotorcraft, Helicopter, Tilt-rotor, UAV, Rotor, Propeller.

Advantages

  • Accurate numerical prediction of performance and of noise generated by rotors and propellers. Acoustic codes coupled with aerodynamic codes (CFD or other methods) for optimised performance.
  • Design, manufacture and wind-tunnel tests of instrumented propeller or rotor models.

Testing

  • Validation of concepts and quantification of design improvements using wind-tunnel tests (including acoustic measurements).
  • Influence of new 3D designs and innovative devices on dynamics (e.g. blade deformations), aerodynamics (e.g. blade loads and wakes) and their consequences on acoustics, can be analysed using a comprehensive understanding of physical phenomena involved.

Simulation

  • Computation of noise emitted by rotating wings and their performance.
  • Detailed analysis of resulting noise emissions.

Expertise

  • Proposal of new designs with analysis of parameters influence.
  • Expertise on both passive and active concepts including numerical design, model manufacture and wind tunnel tests.
  • Design of new rotary concepts using efficient noise prediction codes.


ERATO rotor (Ø 2 meters) -3.5 to -7 dBA noise. [Cooperation with DLR]

 

Experts :

Philippe Beaumier
Yves Delrieux