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Finite volume simulations of turbulent boundary layer flow over anaxisymmetric hill are performed for $Re_H$ = 6500 using Morphing ContinuumTheory (MCT), and compared with DNS data from Castagna et. al. and experimentaldata obtained by Simpson. The inlet profile was specified by inputting valuesfrom the profile specified by Castagna et. al. Root- mean-square velocityfluctuations are inputted using the new variable of gyration from MCT.Additional terms introduced by MCT lead to a new formulation of theQ-criterion, which allows for the visualization of three-dimensional turbulentstructures including a hairpin vortices. Streamline plots of the separationbubble show a more confined bubble than Castagna et. al., but agree well on theseparation and reconnection points. The surface pressure coefficient matchesSimpson much more closely than Castagna et. al. MCT data was obtained on a$6.72 \times 10^6$ cell mesh containing a smaller number of cells by an orderof magnitude than that of the DNS mesh of $5.4 \times 10^7$ by Castagna et. al.The effects of the particle on the larger structures are inferred from thevariation in the new variable of gyration.

A Morphing Continuum Simulation of Transonic Flow over an Axisymmetric Hill