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 process of propane diffusion combustion in a plane jet at the exit of a long nozzle under the acoustic effect
Visualization of Mechanical Processes
2735
Combustion of a turbulent jet with top-hat mean velocity profile with the flame lifted from the nozzle exit (outflow velocity is 15 m/s, Reynolds number is about 5100)
Visualization of Mechanical Processes
3427
Evolution of the jet in the plane where the sinusoidal vortex trail appears and is bifurcated under the effect of the transverse acoustic field with and without acoustic effect
Visualization of Mechanical Processes
2599