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Such flows occur in elements of the gas-dynamic channel of turbojet engines and liquid-fuel rocket engines, ejector pumps, and other technical devices.
      
Velocity field of a liquid stream in a spiral channel of rectangular cross section
      
In intermediate flow conditions, for Knudsen number Kn ~ 1, solutions have been obtained for the limiting cases: an infinitely long channel [4] and a channel of zero length (an aperture) [5].
      
Although their accuracy is acceptable for practical calculations, the equations cannot be used for a physical analysis of the local phenomena occurring in the working channel of a plasma generator.
      
The basis of the computational method is a quasi-one-dimensional gasdynamic model of the flow of an electrically conducting gas in the channel of the plasma generator developed and studied in [2].
      
A system of differential equations describing small perturbations of the steady flow of a non-viscous ideal gas in a channel of variable cross section is analyzed in this paper.
      
Heat transfer in the channel of a high-power MHD generator
      
On the theory of flow of an incompressible viscous fluid in a channel of arbitrary section
      
The wave process in a channel of variable section is investigated numerically, its characteristics found, and a comparison made with the linear theory.
      
Calculation of the flow within the channel of an axisymmetric entrance diffuser
      
One of the possible flow schemes within the channel of a supersonic axisymmetric entrance diffuser is considered.
      
Axisymmetric flow in the channel of such a diffuser is calculated in the presence of an oblique shock in front of the separation region formed at the corner of the central body.
      
On the optimal distribution of the flow rate of gas blown through the side walls of the channel of a de plasmotron (plasma gener
      
It is well known that the blowing of cold gas through the side walls of the channel of a dc plasmotron (plasma generator) with longitudinal blowing over the arc leads to an increase in the useful power of the plasmotron [1].
      
The present paper solves the problem of the optimal distribution of the flow rate of gas blown through the side walls into the channel of a dc plasmotron of arbitrary shape F(x).
      
A solution is presented to the problem of the laminar flow of a heat-transfer vapor in an annular channel of constant cross section in the presence of a liquid film on the outer wall and heating through the inner wall of the channel.
      
Motion of shock waves in a channel of variable cross section in the presence of a steady flow regime
      
The motion of shock waves against a steady flow in a channel of variable cross section is considered.
      
Investigation of isothermal flow of a mixture of gas and particles in a channel of variable section
      
Hydraulic models of flow in the channel of an mhd generator based on the equations of a two-dimensional boundary layer
      
 

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