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.
Original language | English |
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Pages (from-to) | 149-152 |
Number of pages | 4 |
Journal | Thermophysics and Aeromechanics |
Volume | 25 |
Issue number | 1 |
DOIs | |
Publication status | Published - 1 Jan 2018 |
Keywords
- duct
- Euler and Navier−Stokes equations
- jet
- near-wall energy sources
- supersonic flow