ERD

Periodic Reporting for period 2 - INVENTOR (INnoVative dEsign of iNstalled airframe componenTs for aircraft nOise Reduct...

Project: INVENTOR

Updated at: 31-05-2024

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Project acronym INVENTOR

Parametric study on slat noise reduction and selection of best NRTs based on porous treatments

Project: INVENTOR

Updated at: 29-02-2024

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Project acronym INVENTOR

Parametric study on slat track noise generation and mitigation and selection of best low-noise slat track designs

Project: INVENTOR

Updated at: 29-02-2024

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Project acronym INVENTOR

A direct-hybrid CFD/CAA method based on lattice Boltzmann and acoustic perturbation equations

Project: INVENTOR

Updated at: 31-10-2023

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Project acronym INVENTOR

Effect of Deflection Angle on the Noise and Aerodynamic Loads Generated by a Wall-Mounted Flat Plate

Project: INVENTOR

Updated at: 31-10-2023

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Project acronym INVENTOR

Multi-chamber micro-perforated panel absorbers optimised for high amplitude broadband absorption using a two-point imped...

Project: INVENTOR

Updated at: 31-10-2023

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Project acronym INVENTOR

Numerical modeling of a wire mesh for aerodynamic noise reduction

Project: INVENTOR

Updated at: 31-10-2023

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Project acronym INVENTOR

Landing Gear Noise Mitigation by an upstream installed Fairing

Project: INVENTOR

Updated at: 31-10-2023

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Project acronym INVENTOR

Parametric study of the effect of slat track geometry on noise emissions

Project: INVENTOR

Updated at: 31-10-2023

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Project acronym INVENTOR

Numerical Simulations of a Landing Gear with Flow Through Fairings for Noise Mitigation

Project: INVENTOR

Updated at: 31-10-2023

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Project acronym INVENTOR

Aerodynamic characterisation of porous fairings: pressure drop and Laser Doppler Velocimetry measurements

Project: INVENTOR

Updated at: 31-10-2023

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Project acronym INVENTOR

Flow Control and Passive Low Noise Technologies for Landing Gear Noise Reduction

Project: INVENTOR

Updated at: 31-10-2023

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Project acronym INVENTOR

The implementation of air curtains on realistic aircraft nose and main landing gear

Project: INVENTOR

Updated at: 31-10-2023

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Project acronym INVENTOR

Air Curtain Design for Landing Gear Noise Reduction

Project: INVENTOR

Updated at: 31-10-2023

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Project acronym INVENTOR

Report on specifications for experimental (AAWT/UoB) and numerical studies on porous slat noise in WP4

Project: INVENTOR

Updated at: 31-07-2023

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Project acronym INVENTOR

Basic structure of the project website

Project: INVENTOR

Updated at: 31-07-2023

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Project acronym INVENTOR

Finalised website

Project: INVENTOR

Updated at: 31-07-2023

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Project acronym INVENTOR

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Periodic Reporting for period 2 - INVENTOR (INnoVative dEsign of iNstalled airframe componenTs for aircraft nOise Reduct...

Parametric study on slat noise reduction and selection of best NRTs based on porous treatments

Parametric study on slat track noise generation and mitigation and selection of best low-noise slat track designs

A direct-hybrid CFD/CAA method based on lattice Boltzmann and acoustic perturbation equations

Effect of Deflection Angle on the Noise and Aerodynamic Loads Generated by a Wall-Mounted Flat Plate

Multi-chamber micro-perforated panel absorbers optimised for high amplitude broadband absorption using a two-point imped...

Numerical modeling of a wire mesh for aerodynamic noise reduction

Landing Gear Noise Mitigation by an upstream installed Fairing

Parametric study of the effect of slat track geometry on noise emissions

Numerical Simulations of a Landing Gear with Flow Through Fairings for Noise Mitigation

Aerodynamic characterisation of porous fairings: pressure drop and Laser Doppler Velocimetry measurements

Flow Control and Passive Low Noise Technologies for Landing Gear Noise Reduction

The implementation of air curtains on realistic aircraft nose and main landing gear

Air Curtain Design for Landing Gear Noise Reduction

Report on specifications for experimental (AAWT/UoB) and numerical studies on porous slat noise in WP4

Basic structure of the project website

Finalised website