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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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[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
[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
ID: AERO0025
Start date: 1990-09-01, End date: 1993-02-28
The major goal of this study is to improve the safety and the fatigue life of aircraft structures which are subjected to sonic excitation. The study is focused on 3 specific objectives: Elaboration of acoustic fatigue strength data for advanced materials. Development of sem...
Programme: FP2-AERO 0C
Record Number: 17199
Last updated on: 1992-11-18
ID: AERO0010
Start date: 1990-01-01, End date: 1992-12-31
To bring about substantial reduction of the noise emission of helicopters and future tilt-rotor aircraft, the corresponding noise prediction capabilities must be considerably improved to provide the European helicopter manufacturers with the necessary competitive edge. Toward...
Programme: FP2-AERO 0C
Record Number: 17191
Last updated on: 1992-11-18
ID: AERO0015
Start date: 1990-02-01, End date: 1992-01-31
Study of the executive software required for use in future Integrated Modular Avionic(IMA) systems and evaluation of the use of ADA language for this purpose.
Programme: FP2-AERO 0C
Record Number: 17180
Last updated on: 1992-11-18
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
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List retrieved on: 2018-01-21
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