Drag of freely rotatable cylinder/splitter-plate body at subcritical Reynolds number

A study examined how the drag coefficient of a circular cylinder is affected by a freely rotatable splitter plate and how the drag compares to the case where the splitter plate is fixed at zero-degree angle of attack.

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Bibliographic Details
Published in:AIAA journal 1996-11, Vol.34 (11), p.2446-2448
Main Authors: Cimbala, John M, Leon, Jonathan
Format: Article
Language:English
Subjects:
Aerodynamics
Aircraft
Exact sciences and technology
Fluid dynamics
Fundamental areas of phenomenology (including applications)
Jets
Mechanical engineering
Physics
Turbulence control
Turbulent flows, convection, and heat transfer
Wakes
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Description
Summary:A study examined how the drag coefficient of a circular cylinder is affected by a freely rotatable splitter plate and how the drag compares to the case where the splitter plate is fixed at zero-degree angle of attack.
ISSN:0001-1452
1533-385X
DOI:10.2514/3.13412