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
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Two-frequency transverse acoustic excitation in a supersonic jet
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