The mechanisms of unsteadiness in nominally two-dimensional (2-D) shock/turbulent-
boundary-layer interactions (STBLIs) cannot be directly extended to three-dimensional (3-D) …

Shock/turbulent-boundary-layer interactions (STBLIs) are ubiquitous in high-speed flight and
propulsion applications. Experimental and computational investigations of swept, three …

Shock-Wave/Boundary-Layer Interaction (SBLI) is ubiquitous in high-speed air vehicles.
SBLI surface flowfield properties of crossing shocks induced by symmetric Double-Fins …

To facilitate large-eddy simulation (LES) of high Reynolds number, wall-bounded
turbulence, modeling of the near-wall fluxes is necessary to maintain solution accuracy; for …

Backward-facing step (BFS) configurations are relevant to many aerospace applications. An
understanding of the underlying dynamics of such flows can aid in developing suitable …

View Video Presentation: https://doi. org/10.2514/6.2021-2757. vid Shock-separated flows
feature in many aerospace applications and present a particular challenge to numerical …

Shock-wave/turbulent boundary-layer interactions (SWTBLIs) are characterized by
lowfrequency unsteadiness, amplified aerothermal loads, and a complex three-dimensional …

View Video Presentation: https://doi. org/10.2514/6.2021-1553. vid The accurate calculation
of turbulent flow separation from a smooth body remains a challenging problem for …