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Unit-Reynolds-number effects on boundary-layer transition

โœ Scribed by STETSON, KENNETH F.; KIMMEL, ROGER L.


Book ID
121238613
Publisher
American Institute of Aeronautics and Astronautics
Year
1993
Tongue
English
Weight
341 KB
Volume
31
Category
Article
ISSN
0001-1452

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๐Ÿ“œ SIMILAR VOLUMES


Low-Reynolds-number effects in a turbule
โœ C. Y. Ching; L. Djenidi; R. A. Antonia ๐Ÿ“‚ Article ๐Ÿ“… 1995 ๐Ÿ› Springer ๐ŸŒ English โš– 761 KB

Low-Reynolds-number effects in a zero pressure gradient turbulent boundary layer have been investigated using a two-component LDV system. The momentum thickness Reynolds number Ro is in the range 400 to 1320. The wall shear stress is determined from the mean velocity gradient close to the wall, allo