SUPIN Supersonic Inlet Design and Analysis Tool (Version 2024A, April 2024)(LEW-20136-1)

The SUPIN Supersonic Inlet Design and Analysis Tool performs design and analysis of axisymmetric pitot, three-dimensional pitot, axisymmetric-spike, two-dimensional, and streamline-traced inlets using an input data file consisting of input factors. SUPIN writes an output data file containing inlet performance metrics and geometric data. The inlet performance metrics calculated include the flow rates, total pressure recovery, and drag. SUPIN can create the surface grids for the inlets that may be used to visualize the inlet geometry, as well as, generate volume grids for computational fluid dynamics (CFD) simulations. SUPIN can also automatically generate three-dimensional, multi-block structured grids for CFD simulations.