Published in Applied Mechanics and Materials, Volume 553, May 1, 2014, pages 205-210.
At the time of publication, author Graham Doig was not yet affiliated with Cal Poly.
The definitive version is available at https://doi.org/10.4028/www.scientific.net/AMM.553.205.
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.
2014 Sage Publications.