Fig. 6

Effect of eccentricity ratio on pressure distribution along circumferential direction at bearing mid-plane for concave axial variation of the bearing geometry at \({{\Phi = 0\,\,and\,\,S_{o} } \mathord{\left/ {\vphantom {{\Phi = 0\,\,and\,\,S_{o} } {D = 1}}} \right. \kern-0pt} {D = 1}}\).