Accession Number:
AD1027283
Title:
Boundary-Layer Bypass Transition Over Large-Scale Bodies
Descriptive Note:
Technical Report,01 Sep 2013,31 Aug 2016
Corporate Author:
UNIVERSITY OF SHEFFIELD SHEFFIELD United Kingdom
Personal Author(s):
Report Date:
2016-12-16
Pagination or Media Count:
44.0
Abstract:
The results suggest that the mean pressure gradient modifies the shape of the streamwise velocity profile compared to the flat-plate boundary layer. The research showed that the streamwise wavenumber plays a key role in the development of the streaks.
Descriptors:
Subject Categories:
- Fluid Mechanics