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Highly-accurate/reliable WT test demonstration of low-noise innovative MLG configuration (ARTIC)
Date du début: 1 juil. 2014, Date de fin: 31 déc. 2015,
The objective of the activity under this CfP is the test of a full-scale Main Landing Gear fuselage-mounted architecture sized for a high-wing regional aircraft configuration in a Wind Tunnel facility. This proposal considers a complete architecture including all necessary features from an aeroacoustic point of view including: gear struts, wheel pack, bay cavity and doors, fairings and portion of ...
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