this simulation predict the hysteresis phenomena when a buseman airfoil will accelerate above the specific choking mach number and decelerate to sub sonic speed.
the simulations will done with rhoCentralFoam with zero viscosity (Euler-Equations)
At first a coarse mesh with around 50k cells is used.
I would be very interested to see the outcome of your simulations! I looked at some papers and webpages and this is a really interesting topic we could validate here on SimScale.
i knew this paper. Some years ago, i hold a presentation about “Busemann Biplane and its improvements” at class of Helmut Sobieczky at TU Wien.
But, at first i have to run some simulations about “shock tube” cases, finding the right/stable boundary conditions and appropriate Courant Number for the rhoCentralFoam solver.
With this information it is easier starting a more complicated case.
Do you mind sharing your presentation with me? Feel free to inbox me.
I am keeping an eye on your simulation to see how you are setting it up as I never heard of the Busemann Biplanes before. Please keep me up-to-date and we will hopefully see some nice post-processing results from you soon!