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Small amplitude forced pitch oscillations of the aircraft model

This video shows the aircraft model tested in the TsAGI wind tunnel at small-amplitude pitch oscillations in order to obtain the dynamic derivatives.

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: 5004 Article added: 15 February 2018 Article last modified: 15 February 2018 © Copyright 2010-2021 Back to top