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TRIMIS

Enabling optimized disruptive airframe-propulsion integration concepts

ENODISE

Enabling optimized disruptive airframe-propulsion integration concepts

Call for proposal: 
H2020-MG-2019-TwoStages
Link to CORDIS:
Objectives: 

ENODISE is an enabler project aimed at reducing aircraft gaseous and noise emissions by improving the integration of the propulsion system with the airframe. Complex aerodynamic and acoustic engine-airframe interactions are involved, which must be better understood to yield the expected gains. ENODISE will investigate the main propulsion-airframe integration issues at low TRL and build a solid basis of knowledge and methods based on simplified but representative configurations, permitting to assess a variety of integration concepts.

ENODISE will investigate the existence of local/global integration optima via an innovative experimental methodology combined with reduced order modelling and machine learning strategies. Selected configurations will be simulated using methods ranging from low-CPU to high-fidelity. The low-CPU techniques will be employed to verify if the experimentally observed optima can be obtained numerically, and the high-fidelity methods will contribute to the detailed investigation of the aeroacoustic mechanisms in addition to permitting a fine-tuning of the low-cost methods. The work being carried out on relatively low-cost generic configurations, this project will permit spanning a broad parameter space and testing optimization-based robust design methods.

Finally, if the interactions between the flow and acoustic field of the propulsion system with the airframe can be detrimental to aerodynamic performance or noise, they also offer opportunities to explore novel flow and acoustic control strategies, not yet explored in combination with installation effects. ENODISE will implement advanced materials and shape modifications to mitigate the adverse installation effects observed during the first phase of the project. The last objective of this project is thus the inclusion of innovative flow and acoustic control technologies in the optimization loop in order to derive better integration designs with minimal detrimental installation effects.

Institution Type:
Institution Name: 
European Commission
Type of funding:
Lead Organisation: 

Institut Von Karman De Dynamique Des Fluides

Address: 
Chaussee De Waterloo 72
1640 Rhode Saint Genese
Belgium
EU Contribution: 
€570,000
Partner Organisations: 

Stichting Nationaal Lucht En-Ruimtevaartlaboratorium

Address: 
Anthony Fokkerweg 2
1059CM AMSTERDAM
Netherlands
EU Contribution: 
€400,000

Rheinisch-Westfaelische Technische Hochschule Aachen

Address: 
Templergraben
52062 Aachen
Germany
EU Contribution: 
€350,000

Gpu Prime Ltd

Address: 
16 ST THOMAS CLOSE
CAMBRIDGE
CB23 7DN
United Kingdom
EU Contribution: 
€350,000

Universiteit Twente

Address: 
Drienerlolaan 5
7522 NB Enschede
Netherlands
EU Contribution: 
€400,000

Office National D'etudes Et De Recherches Aerospatiales

Address: 
CHEMIN DE LA HUNIERE
91120 PALAISEAU
France
EU Contribution: 
€350,000

Deutsches Zentrum Fr Luft Und Raumfahrt E.v

Address: 
Linder Hoehe
51147 KOELN
Germany
EU Contribution: 
€350,000

Universita Degli Studi Roma Tre

Address: 
Via Ostiense 159
154 Roma
Italy
EU Contribution: 
€350,000

Siemens Industry Software Nv

Address: 
INTERLEUVENLAAN 68
3001 LEUVEN
Belgium
EU Contribution: 
€280,000

Pipistrel Doo Podjetje Za Proizvodnjo Zracnih Plovil

Address: 
GORISKA CESTA 50A
5270 AJDOVSCINA
Slovenia
EU Contribution: 
€400,000

Ecole Centrale De Lyon

Address: 
AVENUE GUY DE COLLONGUE 36
69134 ECULLY
France
EU Contribution: 
€400,000

University Of Bristol

Address: 
BEACON HOUSE QUEENS ROAD
BRISTOL
BS8 1QU
United Kingdom
EU Contribution: 
€400,000

Technische Universiteit Delft

Address: 
STEVINWEG 1
2628 CN DELFT
Netherlands
EU Contribution: 
€400,000
Technologies: 
Development phase:
Development phase: