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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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1
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: AERO0023
Start date: 1990-06-01, End date: 1992-10-31
The development of electrically powered actuators (EPA) for flight controls is considered a major milestone in the progress of the "All Electric Aircraft". The objective of the project is to demonstrate the feasibility of producing an electrically powered primary flight contro...
Programme: FP2-AERO 0C
Record Number: 17204
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: AERO0005
Start date: 1990-01-01, End date: 1992-02-29
The main conclusions of this exercise are the following: - 2D methods are operational for unsteady helicopter flow, and they constitute a useful step in developing 3D algorithms - for a hovering rotor, Euler methods, which capture the rotor wake, give good results for the...
Programme: FP2-AERO 0C
Record Number: 17195
Last updated on: 1990-10-02
1
List retrieved on: 2017-11-22
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