Large Eddy Simulations and modal reconstruction of laminar transonic buffet
Pradeep Moise (1), Markus Zauner (1, 2), Neil Sandham (1) ((1), University of Southampton, (2) ONERA - The French Aerospace Lab)

TL;DR
This study uses Large-Eddy Simulations and modal analysis to investigate laminar transonic buffet mechanisms on an aerofoil, revealing that both laminar and turbulent buffet share the same physical origins.
Contribution
It provides a detailed LES-based analysis of laminar transonic buffet and demonstrates that the underlying mechanisms are consistent across different buffet types.
Findings
Low-frequency mode linked to buffet identified
Flow reconstruction shows boundary-layer separation dynamics
Wake mode analysis connects vortex shedding to buffet phenomena
Abstract
Transonic buffet refers to the self-sustained periodic motion of shock waves observed in transonic flows over wings and limits the flight envelope of aircraft. Based on the boundary layer characteristics at the shock foot, buffet has been classified as laminar or turbulent and the mechanisms underlying the two have been proposed to be different (Dandois et al., 2018, J. Fluid Mech., vol. 18, pp. 156-178). The effect of various flow parameters (freestream Mach and Reynolds numbers and sweep and incidence angles) on laminar transonic buffet on an infinite wing (Dassault Aviation's supercritical V2C aerofoil) is reported here by performing Large-Eddy Simulations (LES) for a wide range of parameters. A spectral proper orthogonal decomposition identified the presence of a low-frequency mode associated with buffet and high-frequency wake modes related to vortex shedding. A flow reconstruction…
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