Benard, Emmanuel and Gaillard, L. and Alziary de Roquefort, T. Influence of roughness on attachment line boundary layer transition in hypersonic flow. (1997) Experiments in Fluids, vol. 22 (n° 4). pp. 286-291. ISSN 0723-4864
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Official URL: http://dx.doi.org/10.1007/s003480050050
Abstract
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 |
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| 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 Other partners > Ecole Nationale Supérieure de Mécanique et d'Aérotechnique - ENSMA (FRANCE) Université de Toulouse > Institut Supérieur de l'Aéronautique et de l'Espace - ISAE Other partners > Université de Poitiers (FRANCE) |
| Laboratory name: | |
| Statistics: | download |
| Total amount of citations (from ISI Web of Science): | 4 |
| Deposited By: | Emmanuel Benard |
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