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Innovative Design of Installed Airframe Components For Aircraft Noise Reduction

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TRM-PMM-3 at M36

INVENTOR Technical Review and Project Management Meeting 3

TRM - PMM 3 at Month 36 – (Chalmers University, Göteborg, Sweden)

Tests of air curtain in AWB on the LAGOON and the the GB-TA-MLG LG

Tests of air curtain in AWB on the LAGOON and the the GB-TA-MLG Landing Gears

September 1st, 2022

 

INVENTOR WP3-WP4 Technical Progress Meeting

INVENTOR WP3-WP4 Technical Progress Meeting
Bristol University (UK)
Bristol Engineers'House
30th and 31th of January 2023

Assessment of flow-through fairings based on innovative numerical simulations

Assessment of flow-through fairings based on innovative numerical simulations

TRM-PMM-2 at M24

INVENTOR Technical Review and Project Management Meeting 2

TRM - PMM 2 at Month 24 – ONERA Châtillon (France)

Second ENODISE Public Workshop (with INVENTOR and DJINN)

Advanced Porous Treatment, Liners and Meta-Materials For Engine and Air Frame Noise Mitigation (Second ENODISE Public Workshop with the participation of DJINN and INVENTOR)

November 7th 2022, RWTH, Aachen (Germany)

Flow-through porous fairings assessed on realistic landing gear by DLR

Porous flow-through fairings for landing gear noise reduction:
experimental acoustic assessment by DLR in AWB windtunnel

Flow-through porous fairings down-selected by TU-Delft

Porous flow-through fairings for landing gear noise reduction:
experimental down selection by TU-Delft in A-Tunnel facility

Low noise slat tacks down-selected by NLR

Low noise slat tacks : experimental acoustic down-selection by NLR in in AWT facility

Flow-through porous fairings characterized by VKI and ONERA

Flow-through porous fairings for landing gear noise reduction :
experimental characterization in WAABLIEF (VKI) and B2A (ONERA) windtunnels

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INVENTOR Summary for Publication
Final Dissemination and Exploitation Workshop in Bucharest
TRM-PMM-4 in Bucharest
Numerical simulation of unsteady flow and noise from an academic spoiler configuration
Mitigation of landing gear wake / flap interaction noise
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