𝔖 Bobbio Scriptorium
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Vortex shedding from yawed cylinders.

✍ Scribed by HANSON, A. R.


Book ID
120828508
Publisher
American Institute of Aeronautics and Astronautics
Year
1966
Tongue
English
Weight
383 KB
Volume
4
Category
Article
ISSN
0001-1452

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The vortex shedding in the wake behind linearly tapered circular cylinders has been considered for the two taper ratios 75:1 and 100:1. The Reynolds number based on the velocity of the incoming #ow and the largest diameter was in the range from 130 to 180. The low Reynolds number assured that lamina