Advances in measuring and understanding separated, nominally two-dimensional (2D)
shock-wave/turbulent-boundary-layer interactions (STBLI) have triggered recent campaigns …

Recent advances in shock wave boundary layer interaction research are reviewed in four
areas:(i) understanding low frequency unsteadiness,(ii) heat transfer prediction …

Verification and validation (V&V) are the primary means to assess accuracy and reliability in
computational simulations. This paper presents an extensive review of the literature in V&V …

Laminar–turbulent transition in hypersonic boundary layers has a dramatic effect on heat
transfer, skin friction, and separation. This effect is critical to reentry vehicles and …

Accurate aerodynamic prediction is critical for the design and optimization of hypersonic
vehicles. Turbulence modeling remains a major source of uncertainty in the computational …

Compressibility, Turbulence and High Speed Flow introduces the reader to the field of
compressible turbulence and compressible turbulent flows across a broad speed range …

Direct numerical simulation and inviscid linear analysis are used to study the interaction of a
normal shock wave with an isotropic turbulent field of vorticity and entropy fluctuations. The …

Well-resolved large-eddy simulations (LES) are performed in order to investigate flow
phenomena and turbulence structure of the boundary layer along a supersonic compression …

A hypersonic shock wave/turbulent boundary layer interaction (STBLI) is investigated using
direct numerical simulation (DNS). The geometry is an 8∘ compression ramp, and the flow …

SHOCK/BOUNDARY-LAYER interaction is still an important problem for supersonic aircraft
designers. Such phenomena plays an important role both for internal and external …