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Develop and test power efficient actuator concepts for separation flow control at large aerodynamic areas requiring very low actuation energy

Project description

Advancing active flow control technologies for more efficient aircraft

Active control of air flow over aircraft wings can significantly improve aerodynamic performance. The pulsed jet actuator is a particularly promising technology – compared to constant blowing, it can suppress flow separation much more effectively. The EU-funded WINGPULSE project plans to develop and demonstrate advanced pulsed jet actuator concepts for flow separation control. Researchers will target efficiencies that exceed state of the art – the technology should reduce the net mass flow by a factor of at least 3. To achieve its aims, the project will gather experts in wind tunnel testing, large-scale flow control testing and high-fidelity simulations.

Objective

Flow separation on aircraft wings has been notoriously linked with loss of lift and extra drag. Furthermore, the recent development of larger, more efficient Ultra High Bypass Ratio (UHBR) engines requires slat cut backs at the juncture of the engine pylon, which significantly promotes separation at high angles of attack. WP1.5 of Clean Sky 2 (CS2) Large Passenger Aircraft (LPA) Programme has been dedicated to addressing this very issue by developing active flow control (AFC) strategies.
Among the various AFC techniques proposed in the literature, the pulsed jet actuator (PJA) control has been regarded as a particularly promising one as it suppression separation effectively and with much lower mass flow than the continuous blowing actuation. WINGPULSE is specifically designed to unlock the potential of the PJA technique by combining the expertise of UNOTT in wind tunnel experiments, high-fidelity simulations and control design and the cutting-edge infrastructure and expertise of large-scale flow control testing at ILOT. The overarching aim of WINGPULSE is to develop and demonstrate PJA concepts for flow separation control with efficiency beyond the state-of-the-art (reducing the net mass flow by a factor of 3-5. UNOTT and ILOT will bring together their respective expertise in Computational Fluid Dynamics, aerodynamics, high integrity wind tunnel testing and development of novel flow control actuation systems, including pulsed jet actuator systems, to deliver the two models that facilitate the flow control test programme for UHBR integration in Clean Sky LPA WP1.5.3.

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IA - Innovation action

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Call for proposal

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(opens in new window) H2020-CS2-CFP10-2019-01

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Coordinator

THE UNIVERSITY OF NOTTINGHAM
Net EU contribution

Net EU financial contribution. The sum of money that the participant receives, deducted by the EU contribution to its linked third party. It considers the distribution of the EU financial contribution between direct beneficiaries of the project and other types of participants, like third-party participants.

€ 485 210,00
Address
University Park
NG7 2RD Nottingham
United Kingdom

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Region
East Midlands (England) Derbyshire and Nottinghamshire Nottingham
Activity type
Higher or Secondary Education Establishments
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Total cost

The total costs incurred by this organisation to participate in the project, including direct and indirect costs. This amount is a subset of the overall project budget.

€ 485 210,00

Participants (1)

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