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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
[PROJECT] LOWNOX I - LOW EMISSION COMBUSTER TECHNOLOGY
ID: AERO0016
Start date: 1990-02-01, End date: 1992-05-31
The aim is to investigate and assess the pollution emissions of future aero-engines, covering small and large civil engines. This task is considered urgent, since increased pollutant emissions from aircraft are to be expected in future.
Programme: FP2-AERO 0C
Record Number: 17181
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: AERO0007
Start date: 1990-02-01, End date: 1993-09-30
- A new cage windage model was developed from the test conducted on a new test rig. The development of this new rig and its capabilities to reproduce the different lubrication environments of roller and ball bearings permitted to achieve one of the most important task of th...
Programme: FP2-AERO 0C
Record Number: 17197
Last updated on: 1990-10-02
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
ID: AERO0002
Start date: 1990-02-01, End date: 1992-07-31
Laminar to turbulent flow transition is an important aspect in turbomachinery flows. To gain a better understanding of the transition characteristics, measurements of the flow around 3 different types of leading edges (sharp, cylindrical and C4) were made. Hot wire and flow v...
Programme: FP2-AERO 0C
Record Number: 17192
Last updated on: 1990-10-02
1
List retrieved on: 2018-05-21
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