Aerodynamic Validation of Emission Reducing Technologies
The AVERT project will deliver upstream aerodynamics research that will enable breakthrough technology and innovative aircraft configuration leading to a step change in aircraft performance.
The project will contribute towards:
- strengthening the competitiveness of the European manufacturing industry;
- improving the environmental impact of aircraft concerning emissions.
The main objective of the AVERT project is the development and industrialisation of active flow control technologies for application to a realistic configuration, thereby reducing drag significantly.
This research responds to a target set in the ACARE 2020 review for a substantial increase in aircraft cruise lift-to-drag ratio by realising the full potential of new configurations such as the ‘pro-green’ aircraft. Active flow-control technology can attack the two main sources of aircraft drag – profile drag and vortex drag – both directly and by unlocking traditional configuration constraints and altering the focus of many design rules. It is predicted that the combined drag reduction could be up to 10%, thus leading to large reductions in emissions.
Achieving this objective will give the aircraft manufacturers within AVERT confidence that emerging flow control technologies can be industrialised to the point of practical and beneficial application to an aircraft.
AVERT aims for a 10% improvement in cruise lift-to-drag ratio in addition to that promised by the ‘pro-green’ configuration, due to direct reductions in profile drag and by unlocking traditional design constraints to reduce vortex drag.
Several flow control technologies have emerged recently that are considered to show sufficient promise, which might be usefully applied to an aircraft in order to reduce drag, either directly or by enabling variations in design that would result in lower drag. AVERT will investigate this selection of devices further with the development focused closely on industrial application. This activity will link directly with the work on manufacturing and control technologies, and will be constantly reviewed by industrial partners. This industrial review will assess the viability and gross performance benefits of the devices when applied to full-scale aircraft.
The following describes the five technical objectives of the AVERT project:
- Exploration and development of flow-control technologies for high-speed application;
- Exploration and development of flow-control technologies for low-speed application;
- Development of manufacturing and control technologies for sensors and actuators;
- Industrial validation of flow-control technology;
- Industrial assessment of flow-control technologies.
Description of work
Devices suitable for high-speed application include active transition control, passive and active turbulent skin friction, drag reduction and active buffet control.
Devices suitable for low-speed application include those which produce oscillatory blowing in a flap gap, and synthetic and fluidic jets for controlling flow separation at the leading edge.
The successful industrialisation and application of arrays of flow-control devices onto an aircraft will be highly dependent on the ability to manufacture and install them. Recent advances in MEMS technology (MEMS: microelectromechanical systems) have provided AVERT with the first real opportunity to assess and develop manufacturing processes for large volume production of flow-control devices. Additionally, by drawing on expertise from the field of structural health monitoring, optimisation of the type and distribution of the appropriate devices will be possible, together with the development of advanced means to control them such as open and closed loop systems.
Part of this process will be the validation that the manufacturing processes can deliver arrays of devices in sufficient quantity, quality and durability for industrial application. The final step prior to the inclusion of any of these technologies in the product design process will be a large-scale wind tunnel validation. This will evaluate possible performance gains and provide the final and most rigorous set of performance data for industrial assessment.
The expected results are:
- Quantitative performance of each of the high-speed flow-control technologies;
- Identification of promising flow-control technologies for high-speed application through the use of the performance results in an industrial assessment process;
- Specification of the devices selected for industrial validation;
- Quantitative performance results for each of the low-speed flow-control technologies;
- Identification of promising flow-control technologies for low-speed application through the use of the performance results in an industrial assessment process;
- Specification of the devices selected for industrial validation;
- Feasibility studies concerning the manufacturing processes and costs of selected devices;
- Control laws for closed loop actuator systems;
- Optimisation tools for signal specification and array design for devices aimed at T-S instabilities;
- An array, or arrays, of selected devices manufactured to specifications resulting from the device development activity;
- Testing of these devices to measure their quality, performance and durability;
- Modification of one low-speed wind tunnel model and one high-speed wind tunnel model to incorporate selected devices;
- Test results from wind tunnel tests of the modified models;
- Validated performance characteristics of the selected devices.
- Related Info
- Acronym: AVERT
- Name of proposal: Aerodynamic Validation of Emission Reducing Technologies
- Contract number: AST5-CT-2006-030914
- Instrument: STREP
- Total cost: 7 494 957 €
- EU contribution: 3 900 000 €
- Call: FP6-2005-Aero-1
- Starting date: 01/01/2007
- Ending date: 31/12/2009
- Duration: 36 months
- Objective: Competitiveness
- Research domain: Aerodynamics
- Coordinator: Dr Wood Norman Airbus UK Ltd New Filton House UK BS99 7AR BRISTOL
- E-mail: email@example.com
- Tel: +44 (0)117 9364552
- Airbus España S. L. Sociedad Unipersonal ES
- Alenia Aeronautica S.p.A. IT
- Dassault Aviation FR
- EADS Deutschland GmbH - Corporate Research Center Germany DE
- Deutsches Zentrum für Luft- und Raumfahrt e. V. DE
- National Institute for Aerospace Research 'Elie Carafoli' RO
- Office National d'Etudes et de Recherches Aérospatiales (ONERA) FR
- Paragon Ltd GR
- Vyzkumny a zkusebni letecky ustav, a.s. CZ
- Technische Universität Berlin DE
- Centre National de la Recherche Scientifique, Délégation Régionale 18 FR
- Universidad Politécnica de Madrid ES
- University of Manchester UK
- University of Nottingham UK
- Centre National de la Recherche Scientifique (CNRS) FR