Abstract
The transonic mode of gas flow has significant differences in comparison with both subsonic and supersonic regimes, combining both their general properties and specific features inherent in each of them, the possibility of penetration of weak disturbances upstream in subsonic flows. The behavior of small disturbances in subsonic and supersonic flows is qualitatively different. The paper proposes new analytical model for the mathematical modeling of unsteady transonic flows, including the effect of weak viscosity.
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