Shock buffet on wings encountered in edge-of-the-envelope transonic flight remains an
unresolved and disputed flow phenomenon, challenging both fundamental fluid mechanics …

The physical mechanism governing the onset of transonic shock buffet on swept wings
remains elusive, with no unequivocal description forthcoming despite over half a century of …

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 …

This paper examines the three-dimensional cellular patterns appearing on wings in
subsonic stall and transonic buffet conditions. Unsteady Reynolds-averaged Navier–Stokes …

Self-sustained shock wave oscillations on airfoils, commonly defined as shock buffet, can
occur under certain combinations of transonic Mach numbers M∞ and angles of attack …

Fully three-dimensional (3D) global stability analysis (GSA) is performed on the NASA
Common Research Model at turbulent transonic buffet conditions. The framework here …

The aerodynamics of transport aircraft at the borders of the flight envelope is characterized
by complex interactions and nonlinear, unsteady flow phenomena. The underlying physical …

Transonic buffet is undesirable because it causes vibration, and constraining buffet is crucial
in transonic wing design. However, there is still a lack of accurate and efficient buffet …

In the age of globalization, commercial aviation plays a central role in maintaining our
international connectivity by providing fast air transport services for passengers and freight …

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 …