In this study, an aerodynamics simulation of a road vehicle in a steady-state cornering motion is conducted, and the aerodynamic effects of its postural change in the roll direction are discussed. The numerical results indicated an aerodynamic centrifugal force induced by the roll-on. This aerodynamic effect was decomposed into two causes: a revolution of force direction with a rotation of the vehicle's body, and a change in aerodynamic force distribution on the vehicle's body according to changes in flow structures around the vehicle. From a quantitative evaluation, neither factor is negligible in the aerodynamics of the vehicle during steady-state cornering. The side force distribution in the vehicle's longitudinal direction, the pressure changes on the vehicle's body, and the total pressure distributions around the vehicle were visualized, and aerodynamic phenomena were discussed. The changes in flow caused by roll variations were observed mainly around the front wheels. Nomenclature = Slip angle of a vehicle C S = Aerodynamic side force coefficient CS,flow = Aerodynamic side force coefficient induced by a change in flow phenomena CS,lift = Aerodynamic side force coefficient apparently changed by a rotation of lift and side forces C L = Aerodynamic lift force coefficient C pt = Total pressure coefficient CYM = Aerodynamic yaw moment coefficient CS,flow = Aerodynamic yaw moment coefficient induced by a change in flow phenomena C YM,pitch = Aerodynamic yaw moment coefficient apparently changed by a rotation of pitch and yaw moments C = Variation of aerodynamic coefficient C caused by a cornering motion G = Roll stiffness of a road vehicle 2 = Roll angle of vehicle M = Sprung mass of vehicle r = Yaw rate (yaw angular velocity) r' = Nondimensional yaw rate; r' = r / (U/L) U = Running velocity of vehicle u = Forward speed (longitudinal velocity of vehicle); u = U cos v = Slip speed (lateral velocity of vehicle); v = U sin wr,wor = Valuable in cases with and without roll angle