The high-speed fluid–structure interaction (FSI) occurring between a skin panel and a
turbulent shock-boundary layer interaction (SBLI) are investigated with large eddy …

This paper concerns the interaction of an oblique shock wave with a supersonic turbulent
boundary layer over a thin panel surface, leading to shock–boundary layer interaction and …

The response of an impinging laminar shock–boundary layer interaction (SBLI) to
prescribed surface motions is investigated numerically at M∞= 2, R ea= 120,000, and a …

For an aeroelastic system of a two-dimensional elastic panel subjected to an impinging
inviscid oblique shockwave, the nonlinear flutter characteristics are affected by many factors …

The dynamic coupling between a Mach 1.94 shock wave/turbulent boundary layer
interaction (SBLI) and a flexible panel is investigated. High-order numerical simulations are …

View Video Presentation: https://doi. org/10.2514/6.2023-0945. vid Wind-tunnel experiments
were conducted to investigate the effects of swept impinging shock/boundary layer …

This paper concerns the interaction of an impinging shock wave with a supersonic turbulent
boundary layer over several distinct and permanently deformed surfaces, resulting in …

View Video Presentation: https://doi. org/10.2514/6.2023-4134. vid Experiments on a rigid
panel were conducted to characterize the mean and unsteady pressure fields beneath a …

Turbulence, flow separation, and shock dynamics challenge the modeling and analysis of
high-speed aeroelastic behavior. Motivated by this, the importance of modeling the fidelity of …

Fluid–structure interaction of an elastic plate with piezoelectric elements, turbulent
freestream flow at Mach 2.5, and a pressurized cavity is investigated computationally and …