Variational mode decomposition analysis of the relationship between low-frequency shock-wave oscillations and buffet cells
Yuya Ohmichi, Yosuke Sugioka

TL;DR
This paper uses variational mode decomposition to analyze the relationship between low-frequency shock-wave oscillations and buffet cells on a wing, revealing that buffet cell amplitude correlates with boundary layer separation rather than shock oscillations.
Contribution
It introduces VMD-NCS analysis to study nonstationary flow phenomena and clarifies the interaction between shock waves, boundary layer separation, and buffet cells.
Findings
Buffet cell amplitude correlates with boundary layer separation state.
Shock waves influence boundary layer separation but not directly buffet cells.
VMD-NCS effectively analyzes complex unsteady flow data.
Abstract
This study investigates the relationship between low-frequency shock-wave oscillations and buffet cells on the main wing of the NASA common research model. The flow conditions were set at a Mach number of 0.85, Reynolds number of 2.27 10, and angle of attack of 4.82. Buffet cells are cellular patterns with spanwise periodicity that propagate toward the wing tip, with nondimensional frequencies (Strouhal numbers) of 0.2--0.6, higher than those of shock oscillations associated with transonic buffet. However, the physical mechanisms driving buffet cells and their interaction with low-frequency shock motion are not fully understood. This study employs variational mode decomposition-based nonstationary coherent structure (VMD-NCS) analysis applied to unsteady pressure-sensitive paint measurement data. The results reveal that the amplitude of buffet cells is not…
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