The Aerodynamics of a Cornering Inverted Wing in Ground EffectApplied Mechanics and Materials
AbstractFor racing car configurations an inverted wing produces negative lift that allows increased levels of acceleration to be maintained through corners. Routine aerodynamic analysis, however, will typically be in the straight-line condition. A numerical analysis of the inverted T026 wing geometry through the curved path of a constant radius corner was conducted. The asymmetrical properties of the oncoming flow resulted in the introduction of a rolling and yawing moment along the span, as well as side-force. Yaw angle, flow curvature and a velocity gradient resulted in changes to the pressure distribution over the wing surface. Primary vortex behaviour was observed to differ significantly in both direction and structure.
Copyright2014 Sage Publications.
Citation InformationJames Keogh, Graham Doig, Tracie J. Barber and Sammy Diasinos. "The Aerodynamics of a Cornering Inverted Wing in Ground Effect" Applied Mechanics and Materials Vol. 553 (2014) p. 205 - 210
Available at: http://works.bepress.com/gcdoig/12/