Two-dimensional pressure field imaging of an elastic panel executing post-flutter oscillations
Author:
Funder
North Carolina State University
Air Force Office of Scientific Research
Publisher
Elsevier BV
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4. Coe, C.F., Chyu, W.J., 1972. Pressure-Fluctuation Inputs and Response of Panels Underlying Attached and Separated Supersonic Turbulent Boundary Layers. NASA Technical Report.
5. Oscillating shock impinging on a flat plate at mach 6;Currao,2019
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