Abstract A physico-mathematical model of non-equilibrium, primarily, hypersonic flow is proposed. The model is meant for calculating the flow around the aircraft forebody. By taking as an example the solution of the problem on the flat shock wave profile, it is shown that the model being proposed allows the traditional Navier-Stokes-Fourier model to be improved.
The engineering model of non-equilibrium flow
Russian Aeronautics (Iz VUZ) ; 57 , 3 ; 266-271
2014-07-01
6 pages
Article (Journal)
Electronic Resource
English
The engineering model of non-equilibrium flow
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