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Numerics & Experiments on Low-Speed High-Altitude Wings

Projekt: ForschungResearch

Projektdetails

Goal of the project

The study aims at developing Passive Flow Control Devices (riblets, dimples, discrete roughness elements, leading-edge protuberances) for high-altitude, low-Re, low-Ma airfoils using experimental and advanced numerical techniques (Variational Multiscale Method); through the partnership, Sleeves for Passive Flow Control Devices can be prototype-tested in-flight using infrared-thermography.

On the path to these technological objectives, several scientific objectives will be pursued: the development of Variational Multiscale Method, the calibration of transitional RANS models for the flows at hand, the execution of in-flight infrared-measurements at high-altitude.

Role of the organisation

KMS is lead voor all aspects of the project, with the exception of flight tests.

Funding acknowledgement

The project MSP21-02 - NELSHAW is financed under the DFR call.
AkronymNELSHAW
StatusLaufend
Tatsächlicher Beginn/ -es Ende14/02/2231/08/26

Projektbeteiligte

RHID domain

  • MSP

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