The dynamic response of a thin buckled panel in a supersonic wind-tunnel experiment is
investigated. Measured time histories of the panel displacement and velocity show co …

This study assesses the robustness and efficiency of the enriched piston theory approach for
modeling aeroelastic loads in the presence of im**ing shocks. Both stationary and …

Shock wave/boundary-layer interactions represent an extreme loading condition in the
structural design of high-speed flight vehicles. However, the complexity of this problem has …

This study describes the enhancement of a computational framework for
aerothermoelasticity using novel model order reduction techniques and efficient coupling …

Balancing accurate and efficient estimation of aerothermodynamic loads is a significant
challenge for multidisciplinary modeling and analysis of high-speed vehicles. This study …

A framework for uncertainty propagation in hypersonic aeroelastic and aerothermoelastic
analyses is presented. First, the aeroelastic stability of a typical section representative of a …

This study investigates the impact of the high-temperature effect, especially the real gas
effect and chemical reactions, on hypersonic aerothermodynamic solutions of double cone …

This paper describes an effort to apply current structural, thermal, and fluid reduced order
modeling methodologies (ROMs) to multi-disciplinary interaction problems that are of …

This paper presents a novel physics-infused reduced-order modeling (PIROM) methodology
for efficient and accurate modeling of nonlinear dynamical systems. The PIROM consists of a …

A surrogate-based modeling strategy is presented for robust and efficient prediction of
unsteady aeroelastic loads in the presence of shock-induced separation. Enriched piston …