Abstract
Dual-stream nozzle jet computations conducted using different numerical algorithms developed at Zhukovsky Central Aerohydrodynamic Institute (TsAGI) and Keldysh Institute of Applied Mathematics, Russian Academy of Sciences (KIAM RAS) are presented. The scale-resolving approaches of the DES family based on higher accuracy numerical methods are applied. The flow considered is studied experimentally at Khristianovich Institute of Theoretical and Applied Mechanics, Siberian Branch, Russian Academy of Sciences (ITAM SB RAS). The jet is axisymmetric up to the effect of the supporting pylons, cold, subsonic at the inner nozzle exit, and supersonic at the outer nozzle exit. The computational data are compared with the experiment and with each other.
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This work was supported by the Russian Foundation for Basic Research, project nos. 18-08-01436 А and 18-31-00368 mol_а. The results of the Keldysh Institute of Applied Mathematics, Russian Academy of Sciences were obtained using the computing resources of the Kurchatov Institute.
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Bosniakov, S.M., Wolkov, A.V., Duben, A.P. et al. Comparison of Two Higher Accuracy Unstructured Scale-Resolving Approaches Applied to Dual-Stream Nozzle Jet Simulation. Math Models Comput Simul 12, 368–377 (2020). https://doi.org/10.1134/S2070048220030102
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DOI: https://doi.org/10.1134/S2070048220030102