Supersonic Inlet Experiment
grabcad
A simple model, drawn to experiment with design tables. This is a converging-diverging inlet, with its dimensions controlled by the design table. The user can input the inlet mach number and inlet diameter, and the design table will use compressible flow theory to calculate the proper throat area. A great experiment for anyone wanting to play around with solidworks flow simulation... Try it with frictionless walls, and the simulation is accurate, add friction and see how boundary layer effects cause problems. Remember to follow the instructions in the design table!
With this file you will be able to print Supersonic Inlet Experiment with your 3D printer. Click on the button and save the file on your computer to work, edit or customize your design. You can also find more 3D designs for printers on Supersonic Inlet Experiment.