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Transonic High Reynolds Number Transition Experiments  in the ETW Cryogenic Wind Tunnel
ONERA.
Airbus.
CIRA.
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2010 (English)Conference paper, Published paper (Refereed)
Abstract [en]

With the goal of studying Natural Laminar Flow (NLF) wings for future ‘green’ transport aircraft, the aim of the European Research Project TELFONA is to develop and demonstrate the possibility of testing full aircraft models with NLF wings at large Reynolds numbers in the cryogenic Wind Tunnel ETW. Two main steps were defined, first the design and test of a ‘calibration’ model, to be followed by a realistic transport aircraft model. This paper is dedicated to the first one, which was especially designed in order to allow a calibration of the Wind Tunnel transition N-factors at large values of the chord Reynolds number typical of testing in ETW. The paper will describe these different phases of the activities, from design, testing and numerical validation, with a focus on the validation and calibration of transition prediction tools. Examples of numerical results obtained by the project partners will be confronted to the experiments. 

Place, publisher, year, edition, pages
2010.
Series
AIAA paper, 2010-1300
National Category
Aerospace Engineering
Identifiers
URN: urn:nbn:se:kth:diva-93994ISBN: 9781600867392 (print)OAI: oai:DiVA.org:kth-93994DiVA: diva2:524821
Conference
48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition 4 - 7 January 2010, Orlando, Florida
Note
QC 20120808Available from: 2012-05-04 Created: 2012-05-04 Last updated: 2012-08-08Bibliographically approved

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http://elib.dlr.de/61758/

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Hanifi, Ardeshir

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