Skip to main content
Go to the home page of the European Commission (opens in new window)
English English
CORDIS - EU research results
CORDIS

Thrust Reverser Unit flow visualization

Project description

New technique to assess nacelle aerodynamics in next-generation engines

Increasing the ratio of airflow that bypasses the engine core is a main tool that aeroengine designers use to improve fuel efficiency. Although ultra-high bypass ratio (UHBR) aeroengine architectures offer increased propulsive efficiencies, they are not without their issues. Challenges mainly relate to the aerodynamics of the isolated nacelle and the interference effects between different engine components. The EU-funded TRUflow project plans to develop novel measurement techniques for visualising and evaluating reverse flow interactions with fan aerodynamics in short and slim engine nacelle designs for next-generation UHBR aeroengines. Wind tunnel tests will be carried out to prove the efficacy of these techniques.

Objective

Thrust Reverser Unit flow visualization – TRUflow will develop novel measurement techniques for the visualization and evaluation of reverse flow interactions with fan aerodynamics in short slim engine nacelle designs applicable to the next generation of ultra-high bypass ratio (UHBR) aero engines. UHBR engine architectures offer increased propulsive efficiency through operation at reduced specific thrust, enabled by increased engine diameter. This poses challenges, both in terms of the aerodynamics of the isolated nacelle, and the potential for interference effects between the different engine components such as the Thrust Reverser Unit (TRU). TRUflow will initially investigate several visualization techniques using a static demonstrator as a workbench for these measurement techniques. Following this investigation, a Wind Tunnel Test (WTT) will be carried out aiming to prove the efficacy of these techniques. In parallel, TRUflow will develop and verify a numerical methodology for the evaluation of TRU cascades. The numerical and experimental data will be fused together to generate a reduced order model of the TRU unit suitable for design.

Programme(s)

Multi-annual funding programmes that define the EU’s priorities for research and innovation.

Topic(s)

Calls for proposals are divided into topics. A topic defines a specific subject or area for which applicants can submit proposals. The description of a topic comprises its specific scope and the expected impact of the funded project.

Funding Scheme

Funding scheme (or “Type of Action”) inside a programme with common features. It specifies: the scope of what is funded; the reimbursement rate; specific evaluation criteria to qualify for funding; and the use of simplified forms of costs like lump sums.

RIA - Research and Innovation action

See all projects funded under this funding scheme

Call for proposal

Procedure for inviting applicants to submit project proposals, with the aim of receiving EU funding.

(opens in new window) H2020-CS2-CFP08-2018-01

See all projects funded under this call

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.

€ 1 413 423,75
Address
MANTON LANE
MK41 7PF Bedford
United Kingdom

See on map

Region
East of England Bedfordshire and Hertfordshire Bedford
Activity type
Private for-profit entities (excluding Higher or Secondary Education Establishments)
Links
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.

€ 1 413 423,75

Participants (3)

My booklet 0 0