The Aerodynamics of a cornering inverted wing in ground effect

James Keogh, Graham Doig, Tracie J. Barber, Sammy Diasinos

Research output: Contribution to journalConference paperpeer-review

7 Citations (Scopus)


For 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.

Original languageEnglish
Pages (from-to)205-210
Number of pages6
JournalApplied Mechanics and Materials
Publication statusPublished - May 2014
Event1st Australasian Conference on Computational Mechanics, ACCM - 2013 - Sydney, Australia
Duration: 3 Oct 20134 Oct 2013


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