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Influence of roughness on attachment line boundary layer transition in hypersonic flow

Bénard, Emmanuel and Gaillard, L. and Alziary de Roquefort, Thierry Influence of roughness on attachment line boundary layer transition in hypersonic flow. (1997) Experiments in Fluids, 22 (4). 286-291. ISSN 0723-4864

(Document in English)

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Official URL: http://dx.doi.org/10.1007/s003480050050


Attachment line boundary layer transition on swept cylinders is studied in a low enthalpy hypersonic wind tunnel at M(x) = 7.14. Sweep angles of 60 degrees and 70 degrees are used and transition is detected by means of heat flux measurements. The influence on attachment line transition of single 2D-roughness elements, in the form of tripwires or slots, as well as 3D obstacles is determined and the results are analyzed with respect to Poll's criterion.

Item Type:Article
Additional Information:Thanks to Springer editor. The definitive version is available at http://www.springerlink.com The original PDF of the article can be found at Experiments in Fluids website: http://www.springerlink.com/content/aa9285uwwmm5pfn9/
Audience (journal):International peer-reviewed journal
Uncontrolled Keywords:
Institution:French research institutions > Centre National de la Recherche Scientifique - CNRS (FRANCE)
Other partners > ISAE-ENSMA Ecole Nationale Supérieure de Mécanique et d'Aérotechnique (FRANCE)
Université de Toulouse > Institut Supérieur de l'Aéronautique et de l'Espace - ISAE-SUPAERO (FRANCE)
Other partners > Université de Poitiers (FRANCE)
Laboratory name:
Deposited On:07 Sep 2011 09:05

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