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Pulsed jEt actuatoRs for SEparation control of tUrbulent flowS

Project description

Optimising technology that will ensure aircraft go with the flow – and vice versa

Flow separation is one of the most important problems in fluid mechanics and particularly aerospace design and control. When the flow of air 'detaches' from the surface of the aircraft, it results in reduced lift and increased pressure drag. Aside from increasing emissions because of greater fuel burn, it can affect the pilot's ability to control the aircraft in extreme cases. Pulsed jet actuators are a promising technology that can combat and control separation. The EU-funded PERSEUS project will combine numerical modelling and wind tunnel testing to determine the optimal parameters for improved jet pulse actuators.

Objective

This project will combine wind tunnel experiments with numerical simulations and a sensitivity analysis to improve the control authority of pulsed jet actuators (PJAs) to separated turbulent flows over a 2.5D airfoil equipped with a flap. The target of this approach is to determine the minimum net-mass-flux required by pulsed jet actuators to compensate for the momentum deficit in the boundary layer. Controlling separation contributes to a decrease in the energy demand, leading to a decrease in CO2 emissions. It also improves the maneuvering capability, safety, and durability of the aircraft by reattaching the boundary layer and suppressing instabilities. The present work considers the sensitivity analysis, using a hierarchy of numerical models, using Reynolds-averaged Navier-Stokes simulations and large eddy simulations for both the flow inner and outer flow. These simulations will be calibrated using wind tunnel experiments by means of a data-assimilation method. The sensitivity analysis will then allow for determining the optimal parameters of the pulsed jet actuators such as operating frequency, output velocity together with their geometry including the actuators’ outflow aspect ratio, chordwise position and inter-actuator distance in the spanwise direction. The selected technology of PJAs will be an improved design of energy efficient fluidic oscillators capable of reaching high outflow velocities with operating frequencies ranging in the natural unstable frequencies of the outer flow. Novel manufacturing techniques such as xurography will also be tested to improve the cost and fabrication time of the PJAs, as well as their integration on the wing. Furthermore, the project will investigate the manufacturing and flow-control capabilities of dual-frequency fluidic oscillators, which may allow for further decreasing the net-mass-flux of the actuators by triggering instabilities with greater potential in altering boundary-layer separation.

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Programme(s)

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Topic(s)

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Funding Scheme

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RIA - Research and 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

UNIVERSITE D'ORLEANS
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.

€ 294 500,00
Address
CHATEAU DE LA SOURCE
45067 Orleans Cedex 2
France

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Region
Centre — Val de Loire Centre — Val de Loire Loiret
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.

€ 294 500,00

Participants (3)

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