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Experimental TRansonic Investigations On Laminar flow and Load Alleviation

The proposal tackles the CfP JTI-CS-2012-1-GRA-02-019. Within the project a Wind-Tunnel-Model is designed, built and tested that is capable of being tested with two main purposes: - access the extend of laminarity on the wing - ev... ver más

31/12/2016

IBK Innovation Gmb...

4M€

Presupuesto del proyecto: 4M€

Líder del proyecto

IBKINNOVATION GMBH CO. KG No se ha especificado una descripción o un objeto social para esta compañía.

TRL 4-5

Fecha límite participación Sin fecha límite de participación.

Ver 4 Participantes

Financiación concedida El organismo FP7 notifico la concesión del proyecto el día 2016-12-31 No tenemos la información de la convocatoria

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No hay información privada compartida para este proyecto. Habla con el coordinador.

4 Participantes

IBK Innovation GmbH&Co. KG

0.00€ | Lider

FOI

N.D. | Participante

UNIVERSITY OF BRISTOL

N.D. | Participante

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Líder del proyecto

IBKINNOVATION GMBH CO. KG No se ha especificado una descripción o un objeto social para esta compañía.

TRL 4-5

Presupuesto del proyecto 4M€

Fecha límite de participación Sin fecha límite de participación.

Descripción del proyecto The proposal tackles the CfP JTI-CS-2012-1-GRA-02-019. Within the project a Wind-Tunnel-Model is designed, built and tested that is capable of being tested with two main purposes: - access the extend of laminarity on the wing - evaluate the performance of LC&A system in the trailing edge of the wing In order to do this the project tackles different points: - a model design is performed that creates a wind-tunnel model with an elastic behaviour comparable to the full-scale wing. This model is as big as possible, although fulfilling all specifications in terms of wind-tunnel restrictions (size, maximum force) in order to allow a hig Reynolds-Number and therefore allow to assess the laminar extend on the wing during the tests in a way that the results are comparable to the full-scale tests. - a first possible LC&A solution which is input to the project is evaluated and optimized and compared with a solution, that was newly designed and optimized LC&A within the project. The best solution is scaled down to model scale and implemented into the model. Within the tests step/ gaps and contaminats are introduced to the model in order to evaluate the stability of the laminar behaviour of the wing with respect to this parameters. In the second test-phase the LC&A devices are used in order to modify the load-distribution on the wing. Before testing the model-wing a ground-vibration test is performed in order to show that the model can be operated safely in the wind-tunnel.

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