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Horizon 2020 project information and now also report summaries are available on CORDIS. All H2020 projects can be downloaded from the EU Open Data Portal .

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ID: AERO0017
Start date: 1990-02-01, End date: 1992-04-30
Development and demonstration of an optical system of sensors for aircraft, based on advanced optical fibre technology. Pressure and acceleration sensors will be investigated. A demonstrating network will be assembled and evaluated providing a set of preliminary results for fo...
Programme: FP2-AERO 0C
Record Number: 17182
Last updated on: 2000-03-10
ID: AERO0018
Start date: 1990-02-01, End date: 1992-03-31
Computational Fluid Dynamics (CFD) is now well established as an integral part of the aerodynamic design process within the aerospace industry. Computer codes for modelling either simple geometries or flows are now mature and in routine use by aerodynamic engineers. The curren...
Programme: FP2-AERO 0C
Record Number: 17183
Last updated on: 1992-11-18
[PROJECT] EUROVAL - VALIDATION OF CFD CODES
ID: AERO0014
Start date: 1990-02-01, End date: 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
ID: AERO0021
Start date: 1990-04-01, End date: 1992-06-30
The purpose is to investigate both experimentally and theoretically the tip clearance effects in advanced axial flow compressors. This investigation aims to produce adequate theoretical models, which will be incorporated in future industrial design systems, thus leading to hig...
Programme: FP2-AERO 0C
Record Number: 17179
Last updated on: 1992-11-18
ID: AERO0009
Start date: 1990-04-01, End date: 1992-06-30
Increasing importance is being attached to the role of helicopter health and usage monitoring to improve the safety of civil helicopters. The application of advanced technologies for health and usage monitoring will have a major impact upon achieving this goal. The 4 Europea...
Programme: FP2-AERO 0C
Record Number: 17190
Last updated on: 1992-11-18
ID: AERO0022
Start date: 1990-07-01, End date: 1993-08-31
For improving the efficiency of new and existing transport aircraft for higher Mach numbers (M = 0.8+), the installation of ducted propfans can play a major role in the future. Preliminary limited investigations in national and international programmes have shown promising res...
Programme: FP2-AERO 0C
Record Number: 17203
Last updated on: 1992-11-18
[PROJECT] ELFIN I - Laminar flow technology
ID: AERO0013
Start date: 1989-12-01, End date: 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
Start date: 1990-01-01, End date: 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
ID: AERO0028
Start date: 1990-07-01, End date: 1992-09-30
Initial assessments indicate that active noise control, the introduction of antinoise cancelling the original noise, has a promising potential for solving the critical low frequency interior noise problem of fixed wing and rotary wing aircraft. The main goal of this project ...
Programme: FP2-AERO 0C
Record Number: 17202
Last updated on: 1992-11-18
ID: AERO0011
Start date: 1990-03-01, End date: 1992-02-28
The aim of this project is to produce a computer model capable of predicting the interactional aerodynamic effects between helicopter rotor blades and the fuselage.
Programme: FP2-AERO 0C
Record Number: 17184
Last updated on: 1992-11-18
12 3 > 
List retrieved on: 2018-02-25
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