Large amplitude forced pitch oscillations of the aircraft model
Project: Visualization of Mechanical Processes
Journal: Visualization of Mechanical Processes: An International Online Journal
Topics: Turbulence, Aerodynamics
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.
The jet flow at different distances from the nozzle exit section
Visualization of Mechanical Processes
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Dynamics of separated flow structure behind the semicylindrical rib in the channel at Re=604
Visualization of Mechanical Processes
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The influence of actuators located on the nozzle at 30 mm from the exit on the jet flow in the confined box through the vorticity field
Visualization of Mechanical Processes
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