Let's test some of the ProjectX solvers for the case of a NACA0012 airfoil in compressible, inviscid flow. Each test case starts with an initial primal solution (sample x-momentum shown below). After reading the input, ProjectX runs a particular test case. Subsequently, all numerical data stored in the history (.hist) files are compared with a "true" history file. In some cases, the solvers are also run in parallel using MPI and compared with the solvers run in serial. The drag and lift coefficients along with residual convergence are given. For more information, please consult the .job and .hist files located in the corner of each panel. |