[dss91]

I am looking to do a project for my Gasdynamics course involving modeling the inlet and nozzle of the Concorde, performing a CFD analysis of it (or a slightly simplified model) in ANSYS, and then comparing my results obtained there to a hand calculation method using both oblique/normal shock theory, as well as the thin wave assumption. I am struggling to find anything with regards to the exact dimensions of the inlet or nozzle and was wondering if anyone could point me towards that information.

Thank you,
Derek

[LUQILIN]

Originally Posted by dss91

I am looking to do a project for my Gasdynamics course involving modeling the inlet and nozzle of the Concorde, performing a CFD analysis of it (or a slightly simplified model) in ANSYS, and then comparing my results obtained there to a hand calculation method using both oblique/normal shock theory, as well as the thin wave assumption. I am struggling to find anything with regards to the exact dimensions of the inlet or nozzle and was wondering if anyone could point me towards that information.

Thank you,
Derek

You can try 1D quasi nozzle first.