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Details of Grant 

EPSRC Reference: GR/R90116/01
Title: Understanding of the Fluid Dynamics of Rotor Wake Breakdown in Low Speed Flight
Principal Investigator: Brown, Professor RE
Other Investigators:
Researcher Co-Investigators:
Project Partners:
DSTL
Department: Aeronautics
Organisation: Imperial College London
Scheme: Standard Research (Pre-FEC)
Starts: 01 October 2002 Ends: 30 September 2005 Value (£): 70,459
EPSRC Research Topic Classifications:
Aerodynamics
EPSRC Industrial Sector Classifications:
Aerospace, Defence and Marine
Related Grants:
GR/R90123/01
Panel History:  
Summary on Grant Application Form
Rotor wake breakdown is a potentially dangerous regime of unsteady flow encountered by all helicopters within a range of descending flight conditions. Traditionally flight near the boundaries of the breakdown regime is avoided, but this may no longer be possible with certain advanced rotorcraft shortly to come into service. The physical mechanisms leading to the onset of wake breakdown are poorly understood and the literature is contradictory regarding the effects of rotor geometry and operating condition. A preliminary study has established, though, our ability to model computationally the behaviour of rotors in the breakdown regime, and also to capture the details of the flow experimentally. This work will thus use a synthesis of numerical and wind-tunnel experimentation to expand and validate our detailed understanding of the behaviour of helicopter rotors in the breakdown regime, and will hopefully yield a valid physical model for the onset of wake breakdown which will be of practical use in the development and certification of new and existing rotorcraft.
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Organisation Website: http://www.imperial.ac.uk