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Content archived on 2024-05-28

Low speed aeroacoustic test of an open rotor powered complete model

Objective

Tests will be performed on a full model provided with installed Counter Rotating Open Rotor (CROR) engines. The 1:7 scale model, provided by the Topic Manager, will be mounted on a dorsal sting, located at tunnel centre line. The model is provided with two powered Counter Rotating propellers which are driven by two air motors (owned by the Topic Manager). The model is basically the same as used in L-CROR CTS (JTI-CS-2012-01-SFWA-02-028). However, it will be provided with 2 new engine configurations, new model parts representative of new engine configurations, new nacelle, new pylon and new blades, airframe inflow variations.
The low speed wind tunnel test is offered in the DNW-LLF (Large Low speed Facility) 8m x 6m open test section.
The aim is generating high quality aerodynamic and aero-acoustic data.

Fields of science (EuroSciVoc)

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Programme(s)

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Topic(s)

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Call for proposal

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SP1-JTI-CS-2012-02
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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.

JTI-CS - Joint Technology Initiatives - Clean Sky

Coordinator

STICHTING DUITS-NEDERLANDSE WINDTUNNELS
EU contribution
€ 974 250,00
Address
VOORSTERWEG 31
8316 PR Marknesse
Netherlands

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Region
Oost-Nederland Flevoland Flevoland
Activity type
Research Organisations
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Total cost

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