Aerodynamic Behavior of the X-56A Airfoil During Oscillatory Plunging Motion
The effects of structural motion on the aerodynamics of the X-56A airfoil are investigated experimentally. An oscillatory plunging mechanism provides a sinusoidal plunging motion. The static aerodynamic characteristics of the X-56A airfoil model are verified against computational results from XFLR5...
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| Language: | en_US |
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The University of Arizona.
2016
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| Online Access: | http://hdl.handle.net/10150/621460 http://arizona.openrepository.com/arizona/handle/10150/621460 |