A hypersonic inlet/isolator acts as the “compressor” for scramjet engines through a series of
shocks, which induces complex internal flows. This paper comprehensively reviews the …

A common denominator between conical-symmetry and conical shock interaction is the
spanwise pressure gradient, which perform more non-uniformity and its interaction flow is …

The present paper discusses the physical reliability of turbulence modeling in an adverse
pressure gradient wall flow setup at moderate/high Reynolds number by comparing wall …

The current study discusses how numerical schemes and discretization approaches affect
wall-resolved and wall-modeled LES outcomes. A turbulent boundary layer setup over a flat …

URANOS, a massively parallel GPU-accelerated compressible flow solver for high-fidelity
modeling of compressible wall flows, is presented. URANOS is based on modern high …

The present work compares 2D and 3D CFD modeling of wind turbine blades to define
reduced-order models of eroded leading edge arrangements. In particular, following an …

The current work presents an innovative numerical technique for high-Reynolds/high-Mach
number compressible flow simulations in complex configurations. In particular, the research …

The work describes a systematic optimization strategy for designing hypersonic inlet intakes.
A Reynolds-averaged Navier-Stokes database is mined using genetic algorithms to develop …

Ramjet propulsion is commonly preferred to power supersonic and hypersonic vehicles for
cruising faster than Mach 3. This is an elegant solution owing to the lean architecture which …

Boundary layer instabilities and shock–boundary-layer interactions (SBLIs) critically affect
the performance and safe operation of mixed-compression air intakes. We present a …