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Large amplitude forced pitch oscillations of the aircraft model

This video shows the aircraft model tested in the TsAGI wind tunnel at large-amplitude forced pitch oscillations in order to investigate the dynamic effects of flow separation on the unsteady aerodynamic characteristics.

Read more in Experimental investigation and mathematical simulation of unsteady aerodynamic characteristics of a transonic cruiser model at small velocities in a wide range of angles of attack.

Number of views: 5709 Article added: 15 February 2018 Article last modified: 15 February 2018 © Copyright 2010-2021 Back to top
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