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Le informazioni sui progetti di Orizzonte 2020 e ora anche le relative sintesi delle relazioni sono disponibili su CORDIS. Tutti i progetti H2020 possono essere scaricati dal Portale Open Data dell'UE .

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This project specified and designed a wind tunnel tool to investigate the aerodynamic problems induced by the interaction of engine slipstream and airframe at high subsonic to transonic speeds. This tool was a large modular generic wind tunnel model, powered with air turbines ...
Programme: FP2-AERO 0C
Record Number: 8402
Last updated on: 1996-09-20
[SINTESI DELLA RELAZIONE] Laminar flow technology
The European laminar flow investigation (ELFIN) project focuses on laminar flow research for aircraft wing and nacelle applications. ELFIN research focuses on basic flow investigation. Large scale wind tunnel tests with hybrid laminar flow (HLF) wings and nacelles and flight t...
Programme: FP2-AERO 0C
Record Number: 8400
Last updated on: 1996-09-27
[SINTESI DELLA RELAZIONE] Wind tunnel testing of hybrid laminar flow
A large scale model with boundary layer suction for hybrid laminar flow (HLF) control was designed with tested in the Office National d'Etudes et de Recherches Aerospatiales (ONERA) SIMA wind tunnel. A suction panel on the glove (main suction system (MSS) has been designed an...
Programme: FP2-AERO 0C
Record Number: 8401
Last updated on: 1996-09-27
[PROGETTO] ELFIN I - Laminar flow technology
ID: AERO0013
Data di inizio: 1989-12-01, Termine: 1992-05-31
The reduction of aircraft drag is of major interest to the aeronautical industry. Drag reduction provides clear economic benefits in terms of fuel savings, extended operational range and/or increased payload. In addition, reductions in fuel consumption will have a direct benef...
Programme: FP2-AERO 0C
Record Number: 17186
Last updated on: 1992-11-18
ID: AERO0003
Data di inizio: 1990-01-01, Termine: 1992-01-31
The aim of the project is to develop new algorithms for solving the Navier-Stokes equations governing viscous compressible flow for upwind discretization of the advection terms based on multi-dimensional wave decomposition and development of multigrid techniques using solution...
Programme: FP2-AERO 0C
Record Number: 17193
Last updated on: 1992-11-18
The AEROTRACE project provides a substantial amount of quantitative data on aircraft engine emissions of particulates, nitrogen species and hydrocarbons which will contribute to the following: a more complete modelling of engine exhaust plume chemistry; incorporation of trace ...
Programme: FP2-AERO 0C
Record Number: 20504
Last updated on: 1998-06-24
ID: AERO0014
Data di inizio: 1990-02-01, Termine: 1992-03-31
The aim of the project is to improve the quality of existing CFD codes, as well as their range of applicability. Furthermore, and especially to lower costs in design processes, the existing variety of numerical tools needs to be validated against accurate and detailed measurem...
Programme: FP2-AERO 0C
Record Number: 17187
Last updated on: 1992-11-18
A limited range of turbulence models were tested by the use of boundary layer methods in the absence of numerical velocity. Of the turbulence models tested the Johnson-Coakley (JC) model showed the best performance for separating and separated flows whilst the Cebeci-Smith (CS...
Programme: FP2-AERO 0C
Record Number: 10719
Last updated on: 1996-09-27
Multiple investigations have been performed on the main influences that may affect Navier-Stokes solutions such as turbulence modelling, grid effects and wind tunnel correction parameters. It has been shown that the quality of the results obtained indeed may strongly depend on...
Programme: FP2-AERO 0C
Record Number: 10760
Last updated on: 1996-10-23
[SINTESI DELLA RELAZIONE] Helicopter health and usage monitoring
Helicopter health and usage monitoring (HUM) systems have the potential both to improve flight safety and reduce operating costs. The present situation regarding helicopter reliability and maintainability was reviewed, including an assessment of the airworthiness and of the ec...
Programme: FP2-AERO 0C
Record Number: 8489
Last updated on: 1996-10-22
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