Transonic Shock-buffet and Aeroelastic Instability at buffet conditions

Transonic Shock-buffet and Aeroelastic Instability at buffet conditions

Shock buffet is an aerodynamic instability characterized by self-sustained shock oscillations that occurs at transonic Mach numbers and moderate angles of attack on both airfoil and wing configurations. Shock buffet involves shock oscillations and boundary layer separation and re-attachment without any structural excitation. As the shock-buffet oscillations occur at low frequencies, close to the structural natural frequencies of aircraft wings, it excites a structural dynamic response that might result in unstable fluid-structure interactions (FSI). Our research explores the nature and characteristics of shock-buffet on 2D and 3D configurations, aeroelastic interactions at transonic flow conditions where shock-buffet exists, and flutter envelope determination at these conditions. Understating the shock-buffet and transonic FSI phenomena is crucial for the determination of the flight envelope of transonic cruisers and for developing control strategies to mitigate buffet and increase flight envelopes.

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Lior Poplingher’s talk at the 2023 SciTech

 

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Lior Poplingher

Collaborators/alums: Michael Iovnovich

 

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