Transonic region formation at the thermal and gas-dynamic action on a supersonic duct flow
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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.
Keywordssupersonic flow duct near-wall energy sources jet Euler and Navier−Stokes equations
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