Visualization of the boundary layer transition in low-speed flow
Project: Visualization of Mechanical Processes
Journal: Visualization of Mechanical Processes: An International Online Journal
Article: VISUALIZATION OF BOUNDARY LAYER TRANSITION BY VISCOUS OIL
Topics: Aerodynamics, Supersonic flows, Wind Engineering
This movie presents a full set of images from a wind tunnel test combined in an animation. In the test, the 65° delta wing model of 420 mm length and 332 mm span was tested in subsonic wind tunnel at constant flow speed of 50 m/s and varying the angle of attack
Scientific Machine Learning Approaches for Two-Phase Heat Transfer
Tec Talk
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Dynamics of a single deformable droplet in a channel with two different circular cross sections in the y = 0 plane
Visualization of Mechanical Processes
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Deformation of the free surface by the vortices shedding from a circular cylinder (3)
Visualization of Mechanical Processes
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