“…Both He et al and Bruneau, Khadra, and Mortazavi demonstrated the advantages of using higher order numerical solvers to determine time dependant flow features in platoon that are usually omitted by RANS that contribute to the vehicle's lateral instability. However, in terms of the averaged flow features that influence the mean drag measurements, the RANS solver has been shown to reproduce the wake structures and pressure field reasonably well for various aerodynamic studies including Bordei and Popescu (2011), Axerio et al (2009), Soares, Garry, and Holt (2017), Fu et al (2017), Maleki, Burton, and Thompson (2017) and Ebrahim, Dominy, and Leung (2016).…”