Surface flow and aerodynamic drag of Ahmed body with deflectors

This study investigated the surface flow and the aerodynamic characteristics of a 7/10 scale Ahmed model equipped with deflectors at several angles. The experiments were conducted at Reynolds number of 2.45 x 105 based on the model height. A global luminescent oil film skin-friction measurement technique was applied for the flow fields on the slant and base surfaces. The aerodynamic forces of the model were measured to understand the effect of the deflection angle on the aerodynamic characteristics. The pressure was measured and pressure drags acting on the slant and base surfaces were also calculated. The results showed that the drag and lift of the model suddenly dropped at the deflection angle above-5 degrees. The pressure distribution on the slant and base surfaces became flat with a maximum drag reduction of 8% for the model with a deflection angle of 0 degrees. The skin-friction measurement indicated that the drag reduction was connected to the breakdown of the separation bubble and longitudinal vortices on the slant. At the fully separated flow state, the skin-friction results illustrated two small vortices and a counter-clockwise vortex on the slant. Additionally, the wake vortices shifted from horizontal to vertical structures. The relation among the flow fields on the slant surface, flow on the symmetric plan, pressure distribution, and drag was illustrated for the model with different deflection angles.

Automated summary

This study investigated the surface flow and aerodynamic characteristics of a 7/10 scale Ahmed model with deflectors at different angles. Luminescent oil film skin-friction measurement technique was used to study the flow fields on the slant and base surfaces. The results showed that higher deflection angles resulted in a sudden drop in drag and lift, with a maximum drag reduction of 8% at a deflection angle of 0 degrees.