Modal Analysis of Buffet Effects
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Modal Analysis of Buffet Effects Induced by Ultrahigh Bypass Ratio Nacelle Installation
arXiv:2602.16443v2 Announce Type: replace Abstract: Unsteady shock-boundary-layer interaction on the lower surface of a transport-aircraft wing can be caused or amplified by ultrahigh-bypass-ratio underwing nacelle installation. This work analyzes the resulting buffet dynamics on the Airbus XRF-1 configuration at a Mach number of $0.84$, a Reynolds number of $3.3\times 10^6$, and $-4^\circ$ angle of attack using scale-resolving delayed detached eddy simulations and unsteady...