Numerical Study of the HB-2 Standard Model Aerodynamics at Supersonic Velocities

The HB-2 numerical simulation results are presented for the Mach numbers from 1.5 to 3 at angles of attack from –2° to +24°. The calculated results are compared with the experimental data [Vuković, D. and Damljanović, D., 2019] on the force and moment characteristics. The calculations were conducted using the method of splitting in physical processes realized on unstructured grids. The results calculated on hexagonal and prismatic grids are compared.

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Publication Details

Journal
Fluid Dynamics
Published
2025-12-01
DOI
https://doi.org/10.1134/s0015462825602815
Primary Topic
Computational Fluid Dynamics and Aerodynamics
Type
article
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article

Numerical Study of the HB-2 Standard Model Aerodynamics at Supersonic Velocities

D. S. Yatsukhno
Fluid Dynamics
Computational Fluid Dynamics and Aerodynamics
article

Numerical Study of the HB-2 Standard Model Aerodynamics at Supersonic Velocities

D. S. Yatsukhno
article en

Abstract

The HB-2 numerical simulation results are presented for the Mach numbers from 1.5 to 3 at angles of attack from –2° to +24°. The calculated results are compared with the experimental data [Vuković, D. and Damljanović, D., 2019] on the force and moment characteristics. The calculations were conducted using the method of splitting in physical processes realized on unstructured grids. The results calculated on hexagonal and prismatic grids are compared.

Fluid DynamicsVol. 60(6)
Institute for Problems in Mechanics (RU)
Affordable and clean energy
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Computational Fluid Dynamics and Aerodynamics
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Numerical Study of the HB-2 Standard Model Aerodynamics at Supersonic Velocities — D. S. Yatsukhno · Fluid Dynamics (2025) | TGRS Research Map | TGRS