Geodesic
Supersonic flow in axisymmetric channel
Matematičeskoe modelirovanie i čislennye metody, no. 5 (2015), pp. 109-120
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The supersonic flows are implemented in an axisymmetric channel in many technical devices. These flows are in an expanding part of the nozzle or in the working part of supersonic wind tunnel. The method of supersonic flow calculation in an axisymmetric channel is developed. The method is based on the construction of multi-block axisymmetric grid and linearization of boundary conditions on the aerodynamic surfaces. Testing the method has showed good agreement with known experimental data. The method allows predicting the aerodynamic properties of the aerodynamic form, depending on its location in the channel, as well as the effect of the aerodynamic form on the channel walls in the channel.
Keywords: Supersonic flow, axisymmetric channel. 
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     url = {http://geodesic.mathdoc.fr/item/MMCM_2015_5_a7/}
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F. A. Maximov. Supersonic flow in axisymmetric channel. Matematičeskoe modelirovanie i čislennye metody, no. 5 (2015), pp. 109-120. http://geodesic.mathdoc.fr/item/MMCM_2015_5_a7/

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