Artificial viscosity can be combined with a higher-order discontinuous Galerkin finite element
discretization to resolve a shock layer within a single cell. However, when a non-smooth …

The merit of using supercritical CO 2 (scCO 2) as the working fluid of a closed Brayton cycle
gas turbine is now widely recognized, and the development of this technology is now …

In this paper, we provide a perspective on how the field of computational
aerothermodynamics has evolved and make some educated guesses as to where it is …

THE development of computational tools that can faithfully reproduce high-Mach-number
flight conditions is fundamental to improving our ability to realize hypersonic vehicles …

High-order implicit shock tracking (fitting) is a class of high-order, optimization-based
numerical methods to approximate solutions of conservation laws with non-smooth features …

The steps necessary to achieve the strong coupling between a flowfield solver and a
material response solver are presented. This type of coupling is required to accurately …

Abstract The Hypersonic International Flight Research and Experimentation (HIFiRE) 5 flight
experiment by Air Force Research Laboratories and Australian Defense Science and …

Numerical Computation of Compressible and Viscous Flow is written for those who want to
calculate compressible and viscous flow past aerodynamic bodies. As taught by Robert W …

A new floating shock-fitting technique featuring the explicit computation of shocks by means
of the Rankine–Hugoniot relations has been implemented on two-dimensional unstructured …

We utilize the Navier-Stokes equations to study the amplification of perturbations in a three-
dimensional boundary layer subject to continuous stochastic forcing. The freestream …