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Application of constructal theory to prediction of boundary layer transition onset

Abstract:

Accurate transition onset modeling is a fundamental part of modern turbomachinery designs, where bypass transition is the dominant mechanism of transition to turbulence. Despite this situation a range of transition onset models exist primarily based upon both integral and local parameters within the boundary layer. All such transition models have empirical origins. To date the relationships between such models has not been forthcoming and hence lack of physical understanding of the transition...

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Publication status:
Published

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Publisher copy:
10.1115/GT2006-91166

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Journal:
Proceedings of the ASME Turbo Expo 2006, Vol 3, Pts A and B
Volume:
3 PART B
Pages:
1251-1259
Publication date:
2006-01-01
DOI:
URN:
uuid:3658e3b0-a060-428b-af6d-83f58001bca3
Source identifiers:
369512
Local pid:
pubs:369512
Language:
English
Keywords:

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