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 …

View Video Presentation: https://doi. org/10.2514/6.2021-0909. vid This experimental study
explores the fluid-structure interactions occurring between a control surface and the …

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 US Air Force Research Laboratory Structural Sciences Center recently started an
experimental campaign in the Arnold Engineering Development Center von Kármán Facility …

Flow over thin elastic panels that undergo small amplitude vibrations has a common
occurrence in supersonic and hypersonic platforms. The resulting fluid–structure interactions …

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 …

View Video Presentation: https://doi. org/10.2514/6.2021-2926. vid Following the
investigations into the FSI of a thin compliant plate in supersonic flows in our earlier efforts …

View Video Presentation: https://doi. org/10.2514/6.2021-0912. vid Experiments were
conducted to study the fluid-thermal-structural interactions of a compliant panel exposed to …

Fluid–structure interactions were measured between a representative control surface and
the hypersonic flow deflected by it. The control surface is simplified as a spanwise finite …

View Video Presentation: https://doi. org/10.2514/6.2022-0291. vid The paper presents an
investigation of fluid-thermal-structural interaction (FTSI) on a complex geometry in …