Shock tubes have emerged as an effective tool for applications in various fields of research
and technology. The conventional mode of shock tube operation employs a frangible …

We present a discussion on theoretical, experimental, and computational research studies
on Görtler instability and the related transition to turbulence occurring in compressible …

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 …

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 …

This paper reports experimental results of fluid/structure interactions induced by shock
impingement on a clamped-free/clamped-free compliant panel in a Mach 5.8 Ludwieg tube …

The aeroelastic responses and nonlinear behaviors of a two-dimensional panel impinged by
an oscillating Mach stem shock are investigated through theoretical analysis. Through the …

Flow separation induced by the shock-wave/boundary-layer interaction is detrimental to the
performance of a hypersonic inlet. This paper develops a new method to control the shock …

DUE to lightweight requirement of high-speed vehicles, thin, flexible panels are widely used,
which lead to the risks of undesirable aeroelastic problems threatening the structural safety …

This investigation takes an analytical approach to the oscillations of a cantilevered plate
immersed in a hypersonic flow with shock impingement. In particular, we derive a …

View Video Presentation: https://doi. org/10.2514/6.2022-0241. vid This paper reports
experimental results of fluid-structure interactions induced by shock impingement on a …