LEXIS Turbomachinary use case: T106 profile test case

<p>The test case&nbsp;for T106 profile&nbsp;in a linear cascade. Cascade rigs are a way to test in a simple way various turbomachinery blades. Blades are cylindrical, which means equal 2D sections from hub to tip wall, and repeated tangentially according to the specified pitch. In this case, end walls are linear, not cylindrical and not tapered. The dataset contains an</p> <ul> <li>excel file with&nbsp; <ul> <li>description of the airfoil (x, y coordinates in [mm])</li> <li>geometric pitch /chord data, aspect ratio (parallel end walls)</li> <li>entry boundary conditions <ul> <li>total pressure</li> <li>total temperature</li> <li>flow angle</li> </ul> </li> <li>outlet boundary condition&nbsp; <ul> <li>static pressure</li> </ul> </li> <li>Reynold number (120 000)</li> <li>Velocity at the exit (Mach = 0,59</li> </ul> </li> <li>OpenFOAM input files for <ul> <li>serial run (Allrun)</li> <li>parallel run (Allrun_parallel)</li> </ul> </li> <li>PDF file with the description of the case and obtained results</li> </ul>