Distribution of Mach number around a plate at M=1.82 and flow density 2.45∙10-4
Project: Visualization of Mechanical Processes
Journal: Visualization of Mechanical Processes: An International Online Journal
Article: EVOLUTION OF NONLINEAR PANEL FLUTTER OSCILLATIONS
Topics: Gas dynamics, Aerodynamics, Supersonic flows, Visualization techniques, Numerical methods, Stability, Wind Engineering
This movie shows distribution of Mach number around the elastic plate oscillating in uniform flow at Mach number M=1.82 and flow density 2.45∙10-4
Stability failure of a half-wing model at 25 m/s and frequencies ~4.0 and ~9 Hz in the case without disturbance
Visualization of Mechanical Processes
2507
Reinventing the Toilet: a Global Collaboration Turning an Infrastructure into an Appliance
Tec Talk
2587
Design Considerations for Amusement Rides
Tec Talk
2826