Status of onera research on wake vortex in the framework of national activities and european collaboration

Eric Coustols; Laurent Jacquin; Frédéric Moens; Pascal Molton

Status of onera research on wake vortex in the framework of national activities and european collaboration

Eric Coustols
, Laurent Jacquin
, Frédéric Moens
, Pascal Molton

ONERA Office National d'Etudes et Recherches Aerospatiales

Research output: Contribution to conference › Paper › peer-review

Abstract

This document provides a synthesis of recent experimental research studies conducted at ONERA, aiming at a better characterisation of aircraft wake vortex and its control. Thus, either generic, two-engine or four-engine transport aircraft-type models have been considered in existing complementary facilities from ONERA, being the most appropriate for scrutinizing different stages of wake evolution. Main results from several research programmes are discussed. They have been obtained both from National and European activities, although emphasis has been set on the 5^th Framework Programme project "C-Wake: Wake Vortex Characterisation and Control".

Original language	English
Publication status	Published - 1 Dec 2004
Externally published	Yes
Event	European Congress on Computational Methods in Applied Sciences and Engineering, ECCOMAS 2004 - Jyvaskyla, Finland Duration: 24 Jul 2004 → 28 Jul 2004

Conference

Conference	European Congress on Computational Methods in Applied Sciences and Engineering, ECCOMAS 2004
Country/Territory	Finland
City	Jyvaskyla
Period	24/07/04 → 28/07/04

Keywords

Blowing
Catapult
Differential flap setting
Free-flight facility
Wake vortex
Wind tunnel
Wing span loading

Cite this

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title = "Status of onera research on wake vortex in the framework of national activities and european collaboration",

abstract = "This document provides a synthesis of recent experimental research studies conducted at ONERA, aiming at a better characterisation of aircraft wake vortex and its control. Thus, either generic, two-engine or four-engine transport aircraft-type models have been considered in existing complementary facilities from ONERA, being the most appropriate for scrutinizing different stages of wake evolution. Main results from several research programmes are discussed. They have been obtained both from National and European activities, although emphasis has been set on the 5th Framework Programme project {"}C-Wake: Wake Vortex Characterisation and Control{"}.",

keywords = "Blowing, Catapult, Differential flap setting, Free-flight facility, Wake vortex, Wind tunnel, Wing span loading",

author = "Eric Coustols and Laurent Jacquin and Fr{\'e}d{\'e}ric Moens and Pascal Molton",

year = "2004",

month = dec,

day = "1",

language = "English",

note = "European Congress on Computational Methods in Applied Sciences and Engineering, ECCOMAS 2004 ; Conference date: 24-07-2004 Through 28-07-2004",

}

Status of onera research on wake vortex in the framework of national activities and european collaboration. / Coustols, Eric; Jacquin, Laurent; Moens, Frédéric et al.
2004. Paper presented at European Congress on Computational Methods in Applied Sciences and Engineering, ECCOMAS 2004, Jyvaskyla, Finland.

Research output: Contribution to conference › Paper › peer-review

TY - CONF

T1 - Status of onera research on wake vortex in the framework of national activities and european collaboration

AU - Coustols, Eric

AU - Jacquin, Laurent

AU - Moens, Frédéric

AU - Molton, Pascal

PY - 2004/12/1

Y1 - 2004/12/1

N2 - This document provides a synthesis of recent experimental research studies conducted at ONERA, aiming at a better characterisation of aircraft wake vortex and its control. Thus, either generic, two-engine or four-engine transport aircraft-type models have been considered in existing complementary facilities from ONERA, being the most appropriate for scrutinizing different stages of wake evolution. Main results from several research programmes are discussed. They have been obtained both from National and European activities, although emphasis has been set on the 5th Framework Programme project "C-Wake: Wake Vortex Characterisation and Control".

AB - This document provides a synthesis of recent experimental research studies conducted at ONERA, aiming at a better characterisation of aircraft wake vortex and its control. Thus, either generic, two-engine or four-engine transport aircraft-type models have been considered in existing complementary facilities from ONERA, being the most appropriate for scrutinizing different stages of wake evolution. Main results from several research programmes are discussed. They have been obtained both from National and European activities, although emphasis has been set on the 5th Framework Programme project "C-Wake: Wake Vortex Characterisation and Control".

KW - Blowing

KW - Catapult

KW - Differential flap setting

KW - Free-flight facility

KW - Wake vortex

KW - Wind tunnel

KW - Wing span loading

UR - https://www.scopus.com/pages/publications/84893471704

M3 - Paper

AN - SCOPUS:84893471704

T2 - European Congress on Computational Methods in Applied Sciences and Engineering, ECCOMAS 2004

Y2 - 24 July 2004 through 28 July 2004

ER -

Status of onera research on wake vortex in the framework of national activities and european collaboration

Abstract

Conference

Keywords

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