Porpoising is a well-known problem in race cars, able to downgrade performance, manifesting itself as a mainly bouncing oscillation, due to dependency of aerodynamic downforce to ride height. Different switching mechanisms can explain the onset of such self-excited oscillations, in which ground effect plays a crucial role. This study investigates a possible cause of instability occurring in the aerodynamic load enhancement region, just before static stall of the diffuser appears. A preliminary analysis is presented, with the aid of stability maps, based on minimal models including interaction between non-stationary aerodynamic loads and suspension dynamics. The results suggest possible improvements of stability by fine-tuning of structural and aerodynamic coefficients.

Porpoising is a well-known problem in race cars, able to downgrade performance, manifesting itself as a mainly bouncing oscillation, due to dependency of aerodynamic downforce to ride height. Different switching mechanisms can explain the onset of such self-excited oscillations, in which ground effect plays a crucial role. This study investigates a possible cause of instability occurring in the aerodynamic load enhancement region, just before static stall of the diffuser appears. A preliminary analysis is presented, with the aid of stability maps, based on minimal models including interaction between non-stationary aerodynamic loads and suspension dynamics. The results suggest possible improvements of stability by fine-tuning of structural and aerodynamic coefficients.

Daniele Gualdi;Alessandro De Felice;Enrico Stalio;Silvio Sorrentino
2024

Abstract

Porpoising is a well-known problem in race cars, able to downgrade performance, manifesting itself as a mainly bouncing oscillation, due to dependency of aerodynamic downforce to ride height. Different switching mechanisms can explain the onset of such self-excited oscillations, in which ground effect plays a crucial role. This study investigates a possible cause of instability occurring in the aerodynamic load enhancement region, just before static stall of the diffuser appears. A preliminary analysis is presented, with the aid of stability maps, based on minimal models including interaction between non-stationary aerodynamic loads and suspension dynamics. The results suggest possible improvements of stability by fine-tuning of structural and aerodynamic coefficients.
2024
6-set-2024
XXVI Conference of the Italian Association of Theoretical and Applied Mechanics (AIMETA XXVI)
Napoli, Italia
2-6 Settembre 2024
Gualdi, Daniele; De Felice, Alessandro; Stalio, Enrico; Sorrentino, Silvio
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11380/1390168
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