31st International Conference on Equations of State for Matter | |
Simulating flow around scaled model of a hypersonic vehicle in wind tunnel | |
Markova, T.V.^1 ; Aksenov, A.A.^1 ; Zhluktov, S.V.^1 ; Savitsky, D.V.^1 ; Gavrilov, A.D.^1 ; Son, E.E.^1 ; Prokhorov, A.N.^2 | |
Joint Institute for High Temperatures, Russian Academy of Sciences, Izhorskaya 13, Moscow | |
125412, Russia^1 | |
Baranov Central Institute of Aviation Motors Development, Aviamotornaya Street 2, Moscow | |
111116, Russia^2 | |
关键词: Aerodynamic characteristics; Flow charac-teristics; Hydrogen combustion; Numerical investigations; Numerical predictions; Operation conditions; Physical quantities; Wind tunnel experiment; | |
Others : https://iopscience.iop.org/article/10.1088/1742-6596/774/1/012095/pdf DOI : 10.1088/1742-6596/774/1/012095 |
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来源: IOP | |
【 摘 要 】
A prospective hypersonic HEXAFLY aircraft is considered in the given paper. In order to obtain the aerodynamic characteristics of a new construction design of the aircraft, experiments with a scaled model have been carried out in a wind tunnel under different conditions. The runs have been performed at different angles of attack with and without hydrogen combustion in the scaled propulsion engine. However, the measured physical quantities do not provide all the information about the flowfield. Numerical simulation can complete the experimental data as well as to reduce the number of wind tunnel experiments. Besides that, reliable CFD software can be used for calculations of the aerodynamic characteristics for any possible design of the full-scale aircraft under different operation conditions. The reliability of the numerical predictions must be confirmed in verification study of the software. The given work is aimed at numerical investigation of the flowfield around and inside the scaled model of the HEXAFLY-CIAM module under wind tunnel conditions. A cold run (without combustion) was selected for this study. The calculations are performed in the FlowVision CFD software. The flow characteristics are compared against the available experimental data. The carried out verification study confirms the capability of the FlowVision CFD software to calculate the flows discussed.
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