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 …

Global stability analysis is used to analyse the onset of transonic buffet on infinite swept and
unswept wings. This high-Reynolds-number flow is governed by the unsteady Reynolds …

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 …

Transonic buffeting phenomena on a three-dimensional swept wing were experimentally
analyzed using a fast-response pressure-sensitive paint (PSP). The experiment was …

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 objective of the present study is to explain the evolution of the transonic buffet
phenomenon from two-dimensional airfoils to three-dimensional swept wings by a global …

Unsteady pressure fields on a civil aircraft wing near the onset of transonic buffet have been
investigated experimentally to identify flow unsteadiness that relates to the buffet onset …

The transonic buffet is a complex aerodynamic instability that appears on wings and airfoils
at a high subsonic Mach number and/or angle of attack. It consists of a shock oscillation that …

Shock wave oscillations and surface flow fields on unswept-wing and 10 deg swept-wing
models were experimentally investigated in a two-dimensional transonic wind tunnel facility …