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Power effects aerodynamics for a regional turboprop

Project description

Flying regionally and sustainably on agile adaptive wings

Turboprops are the perfect choice for shorter distances and regional coverage. The EU is preparing the next generation of regional aircraft with high-tech performance boosters such as active adaptive wings to optimise aerodynamics, lighter durable materials and innovative manufacturing techniques. The EU-funded PERTURB project under Clean Sky 2 is doing its part with computational fluid dynamics simulations in concert with wind-tunnel testing in a pressurised facility allowing variation of the atmospheric conditions. The turboprop model is furnished with new control surface concepts. These efforts aim to evaluate the wings' response during particularly turbulent air flow conditions, as a building block for the flight test preparations.

Objective

A CFD characterisation of a regional turboprop configuration with particular focus on the Reynolds number dependence of the power effects, both direct (1P forces and moments) and indirect (slipstream) is performed, in concert with a wind-tunnel test in a pressurised facility to allow variation in Reynolds number. The turboprop is furnished with new control surface concepts. Variable Fidelity Modelling (VFM) techniques are used for the CFD characterisation, deploying steady RANS with actuator disk modelling as the low-fidelity approach and unsteady RANS with full propeller blade modelling as the high-fidelity approach. The latter uses a novel coupling between the RANS solver and a Vortex Particle Method to increase the accuracy of slipstream effects without resorting to costly mesh refinement in the propeller wake. A methodology for determining reliable performance data at full scale is developed, using a combination of CFD and wind-tunnel data at atmospheric conditions only, again deploying VFM.

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-CFP08-2018-01

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Coordinator

AIRCRAFT RESEARCH ASSOCIATION LIMITED
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.

€ 1 631 981,25
Address
MANTON LANE
MK41 7PF Bedford
United Kingdom

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Region
East of England Bedfordshire and Hertfordshire Bedford
Activity type
Private for-profit entities (excluding 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.

€ 1 631 981,25

Participants (1)

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