Abstract
The control simultaneous action of a jet and near-wall energy sources on the shockwave structure of a superso-nic flow in the axisymmetric and planar ducts is studied for the purpose of creating a transonic region. The regimes with an extended transonic region are obtained.
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The work was financially supported by the Russian Foundation for Basic Research (Grant No. 17-08-00183) and within the framework of SB RAS Project III.22.6.2.
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Zamuraev, V.P., Kalinina, A.P. Transonic region formation at the thermal and gas-dynamic action on a supersonic duct flow. Thermophys. Aeromech. 25, 149–152 (2018). https://doi.org/10.1134/S0869864318010146
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DOI: https://doi.org/10.1134/S0869864318010146