Influence of blunt-cone tip temperature on the laminar-turbulent transition in hypersonic boundary layers View Full Text


Ontology type: schema:ScholarlyArticle     


Article Info

DATE

2018-07

AUTHORS

D. A. Bountin, Yu. V. Gromyko, S. V. Kirilovskiy, A. A. Maslov, T. V. Poplavskaya

ABSTRACT

In the present paper, we report on the results of a combined experimetal and numerical study of the laminar-turbulent transition at Mach number 5.95 in the boundary layers of 7-deg cones with a small nose-tip bluntness radius (down to 1.5 mm). The tip temperature of the model was varied in the range from 90 to 440 K. It was confirmed that the small nose-tip bluntness substantially shifts the position of the transition in downstream direction. This effect was also retained in testing the models with local heating/cooling of the cone tip. It is shown that for the experimental conditions implemented in the Transit-M wind tunnel, ITAM SB RAS, the local heating of blunt cone tips exerts almost no influence on the position of the transition. The local cooling of the cone tip with R = 1.5 mm leads to a shift of the transition position in upstream direction. More... »

PAGES

483-496

Identifiers

URI

http://scigraph.springernature.com/pub.10.1134/s0869864318040029

DOI

http://dx.doi.org/10.1134/s0869864318040029

DIMENSIONS

https://app.dimensions.ai/details/publication/pub.1110715056


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