SSeMID · Stability and Sensitivity Methods for Industrial Design
Horizon 2020 — Marie Skłodowska-Curie Actions
- Duration
- 2016-01-01 → 2019-12-31
- EU contribution
- €3,900,232
- Participants
- 11
- Scheme
- MSCA-ITN
Lines connect the coordinator with its partners.
Results in brief
Stability and Sensitivity Methods for Industrial Design
Aviation contributes to more than 2% of global greenhouse gas (GHG) emissions and its activity is increasing exponentially. In the absence of further measures, carbon dioxide (CO2) emissions from international aviation are estimated to almost quadruple by 2050 compared to 2010. It is obvious that an increasing environmental concern is everyday more present in the aeronautical community, industry and research centres, having a definite influence on the way the design of the aircraft of the future. Most of the environmental goals have a direct connection with the aerodynamic performance of the aircraft. Current aircraft are much more efficient than their original designs; and although the wing-body-tail configuration is still the standard shape for most subsonic commercial aircraft currently active, aerodynamic parameters have drastically improved. As an example, the lift to drag ratio has increased from 6 to 20, and noise emissions at take-off have been reduced as much as 40dB. Those numbers give an idea of the evolution towards more efficient designs that have been possible as a result of the combination of new methods and tools and a better understanding of the physics involved in flight. But still, the main limitation of current designs is related to unsteadiness; at the limits of the flight envelope, several not yet well understood phenomena occur; high angle of attack and maximum lift, buffet, flutter, transonic effects, turbulence, detached and highly distorted flows, or shock boundary layer interactions. Those phenomena limit the efficiency and security of current aerodynamic performance. Activities considered in SSEMID has allowed to advance in the development of new methods and tools able to understand those complex configurations where unsteadiness and nonlinear effects are dominant; making possible to uncover the underlying physics and to provide means to control them. Additionally, SSEMID has provide doctoral training to 16 new fellows involve in high level research on several scientific fields such as high accuracy simulation, flow stability, sensitivity and flow control techniques, and to apply their research to realistic problems that currently the industrial partners are not able to solve.
Data: CORDIS, © European Union
Project objective
The increasing environmental awareness of the European society has been always present in the aeronautical community, industry and research centres, having a definite influence on the way the aircraft of the future should be. In this line, the ACARE Vision for 2020, a Group of Renowned Personalities in the aeronautical field, has formulated a clear set of requirements for civil transport aircraft operations in order to reach the following specific environmental goals: halving perceived aircraft noise, 50% cut in CO2 emissions per passenger-km and 80% cut in NOx emissions.Many of these goals have a direct connection with the aerodynamic performance of the aircraft; mainly with aerodynamic technologies. Most of the elements of the aerodynamics of conventional aircraft are modelled and understood to some degree but reliable solutions are not available due to new challenges appearing as the technology matures. One of the most common problems is related to stability analysis for configurations in the limits of the flight envelope or when unsteady effects are dominant. This challenge is the object of the research of SSeMID, and is the focus of the international training plan for young engineers employed within the network. The project will provide valuable information for such aerodynamic structures paving the way to its complete industrialization while increasing the academic knowledge regarding instability mechanisms and covering the necessary skills and knowledge to train experts in this area
Original text from CORDIS.
Participants
- UNIVERSIDAD POLITECNICA DE MADRID · MadridCoordinatorSpain
- AIRBUS GROUP LIMITED · LONDONUnited Kingdom
- AIRBUS OPERATIONS LIMITED · BRISTOLUnited Kingdom
- CADENCE DESIGN SYSTEMS BELGIUM · BRUXELLESBelgium
- DEUTSCHES ZENTRUM FUR LUFT - UND RAUMFAHRT EV · KOLNGermany
- IMPERIAL COLLEGE OF SCIENCE TECHNOLOGY AND MEDICINE · LondonUnited Kingdom
- KATHOLIEKE UNIVERSITEIT LEUVEN · LeuvenBelgium
- KUNGLIGA TEKNISKA HOEGSKOLAN · StockholmSweden
- OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AEROSPATIALES · PalaiseauFrance
- THE CHANCELLOR MASTERS AND SCHOLARS OF THE UNIVERSITY OF CAMBRIDGE · CAMBRIDGEUnited Kingdom
- VON KARMAN INSTITUTE FOR FLUID DYNAMICS · Sint-Genesius-RodeBelgium
Links
- View on CORDIS
- DOI: 10.3030/675008
- https://arquivo.pt/wayback/20201230004842/https://www.ssemid-itn.eu/
- https://ec.europa.eu/research/participants/documents/downloadPublic?documentIds=080166e5afe2a90d&appId=PPGMS
- https://ec.europa.eu/research/participants/documents/downloadPublic?documentIds=080166e5afe2b180&appId=PPGMS
- https://ec.europa.eu/research/participants/documents/downloadPublic?documentIds=080166e5b5596ad3&appId=PPGMS
- https://ec.europa.eu/research/participants/documents/downloadPublic?documentIds=080166e5c168f97b&appId=PPGMS
- https://ec.europa.eu/research/participants/documents/downloadPublic?documentIds=080166e5c8ea459d&appId=PPGMS
- https://ec.europa.eu/research/participants/documents/downloadPublic?documentIds=080166e5cc61cf59&appId=PPGMS
- https://ec.europa.eu/research/participants/documents/downloadPublic?documentIds=080166e5cc61eade&appId=PPGMS
Data: CORDIS, © European Union
