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CORNET SIGNED

CORE NOISE ENGINE TECHNOLOGY

Total Cost €

EC-Contrib. €

Partnership

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Outcomes and
results

CORNET project word cloud

Explore the words cloud of the CORNET project. It provides you a very rough idea of what is the project "CORNET" about.

guide engines external careful entropy indirect blade generation exit core acoustic combustors optical stage vanes heard pressure diagnostics rig lean realistic aircraft direct cores accelerate propagate eddy ngvs flow propagation technologies representative combustion turbine horizon speed conventional inherently burn unsteady nox unsteadiness analytical waves captured rows resolution prediction proving danger rate gives combustor nozzle emissions interaction 2020 engine reduce incident emission generating readily noisier noise requirement exceed tool cornet industry injector validated broadband computations fuel simulations optimisation predicted physics

Project "CORNET" data sheet

The following table provides information about the project.

Coordinator	THE CHANCELLOR MASTERS AND SCHOLARSOF THE UNIVERSITY OF CAMBRIDGE Organization address address: TRINITY LANE THE OLD SCHOOLS city: CAMBRIDGE postcode: CB2 1TN website: www.cam.ac.uk contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.
Coordinator Country	United Kingdom [UK]
Project website	http://www.eng.cornet.cam.ac.uk
Total cost	997˙772 €
EC max contribution	997˙772 € (100%)
Programme	1. H2020-EU.3.4.5.5. (ITD Engines)
Code Call	H2020-CS2-CFP01-2014-01
Funding Scheme	CS2-RIA
Starting year	2016
Duration (year-month-day)	from 2016-03-01 to 2019-04-30

Partnership

Take a look of project's partnership.

#	participants	country	role	EC contrib. [€]
1	THE CHANCELLOR MASTERS AND SCHOLARSOF THE UNIVERSITY OF CAMBRIDGE THE CHANCELLOR MASTERS AND SCHOLARSOF THE UNIVERSITY OF CAMBRIDGE Organization address address: TRINITY LANE THE OLD SCHOOLS city: CAMBRIDGE postcode: CB2 1TN website: www.cam.ac.uk contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	UK (CAMBRIDGE)	coordinator	519˙988.00
2	DEUTSCHES ZENTRUM FUER LUFT - UND RAUMFAHRT EV DEUTSCHES ZENTRUM FUER LUFT - UND RAUMFAHRT EV Organization address address: Linder Hoehe city: KOELN postcode: 51147 website: www.dlr.de contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	DE (KOELN)	participant	377˙783.00
3	TECHNISCHE UNIVERSITAT DARMSTADT TECHNISCHE UNIVERSITAT DARMSTADT Organization address address: KAROLINENPLATZ 5 city: DARMSTADT postcode: 64289 website: www.tu-darmstadt.de contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	DE (DARMSTADT)	participant	100˙000.00

Map

Project objective

Lean burn combustor technologies introduced to reduce NOx emissions are proving to be inherently noisier than conventional combustors, generating broadband noise that can be heard external to the aircraft. Without careful design and optimisation, there is a danger the low emission cores will cause the aircraft engines to exceed the Horizon 2020 noise requirement.

The research in the CORNET proposal is aimed at understanding the flow physics involved in the generation and propagation of core noise in low emission cores. It includes both the ‘direct noise’ of combustion, pressure waves generated directly by unsteadiness in the rate of combustion, and the ‘indirect noise’ generated as entropy waves accelerate through the Nozzle Guide Vanes (NGVs) at combustor exit and propagate through turbine blade rows.

Large Eddy Simulations of a combustor with a realistic engine fuel injector operating at representative engine conditions are validated through high-speed optical diagnostics applied to a high-pressure rig. The combustor modelling gives the entropy and acoustic waves incident on the NGVs. The generation of in-direct noise is predicted through unsteady high-resolution computations of the interaction of these entropy and acoustic waves within a high-pressure turbine stage. The new understanding will be captured in an advanced analytical combustion noise prediction tool that can be readily used by industry.

Publications

List of publications.
year	authors and title	journal	last update
2018	Zhi X. Chen, N. Anh Khoa Doan, Shaohong Ruan, Ivan Langella, N. Swaminathan AÂ priori investigation of subgrid correlation of mixture fraction and progress variable in partially premixed flames published pages: 862-882, ISSN: 1364-7830, DOI: 10.1080/13647830.2018.1459862	Combustion Theory and Modelling 22/5	2020-01-22
2018	I. Langella, N. A. K. Doan, N. Swaminathan, S. B. Pope Study of subgrid-scale velocity models for reacting and nonreacting flows published pages: , ISSN: 2469-990X, DOI: 10.1103/physrevfluids.3.054602	Physical Review Fluids 3/5	2020-01-22

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The information about "CORNET" are provided by the European Opendata Portal: CORDIS opendata.