Geodesic
Energy input influence on aerodynamic characteristics and heat flux occuring at 3D supersonic flow past a model aircraft
Matematičeskoe modelirovanie, Tome 35 (2023) no. 2, pp. 105-125.

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Numerical simulation of a viscous heat-conducting supersonic (M=2.5) three-dimensional gas flow past a model aircraft (spherically blunted cylinder with wings and tail fins) with energy input into the area in front of it is carried out. Simulations were performed using unsteady Reynolds-averaged Navier-Stokes equations (URANS) and Spalart-Allmaras (SA) turbulence model. Influence of attack angle, energy input’s parameters and placement on the model’s aerodynamic characteristics (wave drag and lift) and heat flux on its surface is determined.
Keywords: energy input, viscous heat-conducting gas, shock wave, heat flux. 
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Ya. V. Khankhasaeva. Energy input influence on aerodynamic characteristics and heat flux occuring at 3D supersonic flow past a model aircraft. Matematičeskoe modelirovanie, Tome 35 (2023) no. 2, pp. 105-125. http://geodesic.mathdoc.fr/item/MM_2023_35_2_a7/

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