The transient response of a plate and a cavity is investigated in a supersonic wind tunnel
start experiment where the freestream flow inside the test section reaches turbulent flow at …

The aeroelastic response of a plate with supersonic freestream flow on one side and a
shallow cavity on the other to turbulent pressure fluctuations is investigated computationally …

Flight vehicles that operate in the supersonic regime can be subject to adverse fluid–
structure interactions due to their lightweight design. The presence of geometric obstructions …

Supersonic wind tunnel test data is compared with a nonlinear aeroelastic computational
model, considering a freestream flow with Mach nearly 2, coupled cavity, and no-shock …

The paper presents an investigation of fluid–thermal–structural interaction (FTSI) on a
complex geometry in hypersonic flows. The objective is to assess high-fidelity numerical …

In this paper, an implicit partitioned fluid-structure-acoustic interaction method is presented
for predicting nonlinear aeroelastic response of an elastic composite laminated panel …

The potential aerodynamic theory is implemented to model the flow over a flexible panel.
The present study compares the more complete unsteady version of the potential flow theory …

A recent structural model of a plate is extended to include a nonuniform temperature
differential that varies in time using a modal expansion. The nonlinear structural plate model …

THE experimental work was undertaken as a precursor to a wind-tunnel experiment of a
heated plate in a hypersonic flow. It was desired to see if discernible changes in plate …

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 …