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This article has been cited by the following article(s):

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Aerothermoelastic experimental design for the AEDC/VKF Tunnel C: Challenges associated with measuring the response of flexible panels in high-temperature, high-speed wind tunnels

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Transitional shock wave boundary layer interaction over a flexible panel

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Influence of aerodynamic nonlinearity due to static panel-curvature on flutter of panels at transonic and low supersonic Mach numbers

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