Innovating Works

ARA

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Showing 1 to 20 of 35 results
ODIN: Off Design Installed Nacelles AIRCRAFT RESEARCH ASSOCIATION LIMITED participó en un H2020: H2020-CS2-CFP11-2020-01 Ultra-high bypass ratio engines offer propulsive efficiency improvements and potential fuel burn reduction. The associated larger diameter c...
2021-01-12 - 2023-12-31 | Financiado
SUBLIME: Supporting Understanding of Boundary Layer Ingesting Model Experiment AIRCRAFT RESEARCH ASSOCIATION LIMITED participó en un H2020: H2020-CS2-CFP09-2018-02 SUBLIME (Supporting Understanding of Boundary Layer Ingestion Model Experiment) The introduction of engines integrated with the rear fusela...
2019-11-25 - 2023-03-31 | Financiado
PERTURB: Power effects aerodynamics for a regional turboprop AIRCRAFT RESEARCH ASSOCIATION LIMITED tramitó un H2020: H2020-CS2-CFP08-2018-01 A CFD characterisation of a regional turboprop configuration with particular focus on the Reynolds number dependence of the power effects, b...
2019-04-17 - 2022-09-30 | Financiado
TRUflow: Thrust Reverser Unit flow visualization AIRCRAFT RESEARCH ASSOCIATION LIMITED tramitó un H2020: H2020-CS2-CFP08-2018-01 Thrust Reverser Unit flow visualization – TRUflow will develop novel measurement techniques for the visualization and evaluation of reverse...
2019-04-17 - 2022-10-31 | Financiado
COMPACT: COMbined Passive and Active Flow Control Technology Wing AIRCRAFT RESEARCH ASSOCIATION LIMITED participó en un H2020: H2020-CS2-CFP08-2018-01 The aim of this project is to design and manufacture a large Hybrid Laminar Flow Control (HLFC) half model, representative of a civil transp...
2019-04-16 - 2023-12-31 | Financiado
ANTIFOD: A New proTection devIce for FOD AIRCRAFT RESEARCH ASSOCIATION LIMITED participó en un H2020: H2020-CS2-CFP07-2017-02 The main objective of this innovation action is to develop a Foreign Object Debris (FOD) protection device applied to an electrical ECS fres...
2018-10-22 - 2022-01-31 | Financiado
ANACO: Advance Nacelle Aerodynamic Optimisation AIRCRAFT RESEARCH ASSOCIATION LIMITED tramitó un H2020: H2020-CS2-CFP07-2017-02 ANACO will facilitate the multi-objective optimisation of short and slim nacelle design for the next generation of ultra-high bypass ratio (...
2018-10-10 - 2022-11-30 | Financiado
AvAUNT: AdaptiVe Area nozzle for Ultra high bypass Nacelle Technology AIRCRAFT RESEARCH ASSOCIATION LIMITED tramitó un H2020: H2020-CS2-CFP03-2016-01 The AvAUNT proposal seeks to advance the state-of-the-art in understanding of the aerodynamic interference challenges associated with the Ul...
2017-03-07 - 2022-08-31 | Financiado
POLITE: Powered modular Wind Tunnel model for low and high Reynolds tests AIRCRAFT RESEARCH ASSOCIATION LIMITED participó en un H2020: H2020-CS2-CFP02-2015-01 POLITE answers the CfP JTI-CS2-2015-CFP02-REG-02-02, published in the second batch of the JTI-Cleansky 2. Within the work-package linked to...
2016-12-06 - 2019-12-31 | Financiado
RELOAD: Regional turboprop loads control through active and passive technologies AIRCRAFT RESEARCH ASSOCIATION LIMITED tramitó un H2020: H2020-CS2-CFP01-2014-01 A number of active and passive Loads Control and Alleviation concepts and technologies will be proposed, developed and evaluated. Aerodynami...
2016-01-22 - 2019-03-31 | Financiado
LOSPA: Model Design and Manufacturing of the Turbofan Configuration for Low Speed Aerodynamic and Acoustic... AIRCRAFT RESEARCH ASSOCIATION LIMITED tramitó un FP7: "A requirement has been produced to design and manufacture an innovative new wind tunnel model to enable the acquisition of aerodynamic and...
Financiado
IDOHAP: INNOVATIVE DESIGN OF HUBS AND PROPELLERS AIRCRAFT RESEARCH ASSOCIATION LIMITED tramitó un FP7: The IDOHAP proposal is for the detailed design of two CROR models to be installed on an existing wind tunnel test rig. Each model to compris...
Financiado
ENITEP: Experimental and Numerical Investigation of Turbulent Boundary Layer Effects on Noise Propagation in... AIRCRAFT RESEARCH ASSOCIATION LIMITED tramitó un FP7: "A requirement has been produced to perform a combination of experimental wind tunnel tests and numerical simulations to study the phenomena...
Financiado
ADOCHA: Acoustic Design Of High lift Architectures AIRCRAFT RESEARCH ASSOCIATION LIMITED tramitó un FP7: Regulation of the sound production of aircraft is becoming stricter, in part due to an increase in the noise generated due to the rising num...
Financiado
DEAFCON: Wind Tunnel Model Design with Active Flow Control for Low Speed Test AIRCRAFT RESEARCH ASSOCIATION LIMITED tramitó un FP7: "The original requirement covered by this DEAFCON proposal was for the detailed design of two low speed half models, with a fully pressure p...
Financiado
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