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Impact of Energy Input on the Aerodynamic Characteristics and Heat Flux Occurring in the 3D Supersonic Flow Past a Model Aircraft

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Abstract

The impact of the energy input in the region in front of a model aircraft (a spherically blunted cylinder with wings and tail fins) on the structure of a viscous heat-conducting supersonic (M = 2.5) three-dimensional gas flow is numerically simulated. The simulations are performed using the unsteady Reynolds-averaged Navier–Stokes (URANS) equations and the Spalart–Allmaras (SA) turbulence model. The impact of the attack angle, parameters and placement of the energy input on the model’s aerodynamic characteristics (wave drag and lift) and heat flux on its surface is determined.

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Funding

The study was supported by the Russian Science Foundation, project 22-11-00126.

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  1. Keldysh Institute of Applied Mathematics, Russian Academy of Sciences, Moscow, Russia

    Ya. V. Khankhasaeva

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  1. Ya. V. Khankhasaeva
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Correspondence to Ya. V. Khankhasaeva.

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Khankhasaeva, Y.V. Impact of Energy Input on the Aerodynamic Characteristics and Heat Flux Occurring in the 3D Supersonic Flow Past a Model Aircraft. Math Models Comput Simul 15, 765–779 (2023). https://doi.org/10.1134/S2070048223040063

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