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TRIMIS

Low speed aeroacoustic test of large aircraft model with open rotor engines

Project

L-CROR OTS - Low speed aeroacoustic test of large aircraft model with open rotor engines


Funding origin:
European
European Union
STRIA Roadmaps:
Vehicle design and manufacturing (VDM)
Vehicle design and manufacturing
Transport mode:
Airborne
Airbone
Transport sectors:
Passenger transport
Passenger transport
Freight transport
Freight transport
Duration:
Start date: 01/10/2012,
End date: 01/03/2013

Status: Finished
Funding details:
Total cost:
€3 195 000
EU Contribution:
€2 396 250

Overview

Objectives:

Tests were performed on a full model with installed CROR engines. The model was mounted on a dorsal sting, located at tunnel centre line. The model was provided with two powered Counter-Rotating propellers which are driven by two air motors (owned by the Topic Manager). The model was the same model as used in L-CROR-CTS (JTI-CS-2012-01-SFWA-02-028).

The aim of the test was to determine the acoustic characteristics of the full model. Innovative measuring techniques and hardware solutions were used to assess the in-flow and out-of-flow noise signature.

The test will be performed in the 8mx6m open test section of DNW-LLF.

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