Within a narrow band of flight conditions in the transonic regime, interactions between shock-
waves and intermittently separated shear layers result in large amplitude, self-sustained …

SHOCK buffet, also termed shock-induced oscillations, is a transonic flow instability
phenomenon in which a shock wave generated on a lifting surface interacts with a partially …

A robust strategy for the RANS shielding of attached boundary layers in a hybrid RANS/LES
context is presented, addressing two major issues. Firstly, the attached boundary layers …

The self-sustaining mechanisms of shock oscillations in transonic airfoil buffet are studied by
wall-resolved large-eddy simulation (LES) and resolvent analysis. The LES successfully …

The paper presents a computational study of the transonic shock-buffet flow instability
phenomenon on three-dimensional wings. Reynolds-averaged Navier–Stokes simulations …

The objective of this paper is to analyze the 3D buffet phenomenon which appears on a
swept wing at a high Mach number and/or high angle of attack. This aerodynamic instability …

The present experimental investigation characterizes the development and decay of
transonic buffet on the supercritical airfoil OAT15A, as well as the flow field and shock …

, the sound wave propagation in the flow field outside the separation of a transonic buffet
flow at a Mach number M∞= 0.73 and an angle of attack α= 3.5 over a DRA 2303 …

High-fidelity computational modeling and optimization of aircraft configurations have the
potential to enable engineers to create more efficient designs that require fewer unforeseen …

The dynamics of a transonic buffet flow on the suction side of a highly loaded 2-D
compressor blade model is investigated at a chord-based Reynolds number of 1.4 * 10^ 6 …