Stability of a hypersonic shock layer on a flat plateStabilité d'une couche de choc hypersonique sur une plaque plane. |
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Authors: | Anatoly A Maslov Tatiana V Poplavskaya Boris V Smorodsky |
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Institution: | Institute of Theoretical and Applied Mechanic SB RAS, Institutskaya str. 4/1, 630090 Novosibirsk, Russia |
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Abstract: | Stability of a hypersonic shock layer on a flat plate is examined with allowance for disturbances conditions on the shock wave within the framework of the linear stability theory. The characteristics of the main flow are calculated on the basis of the Full Viscous Shock Layer model. Conditions for velocity, pressure, and temperature perturbations are derived from steady Rankine–Hugoniot relation on the shock wave. These conditions are used as boundary conditions on the shock wave for linear stability equations. The growth rates of disturbances and density fluctuations are compared with experimental data obtained at ITAM by the method of electron-beam fluorescence and with theoretical data of other authors. To cite this article: A.A. Maslov et al., C. R. Mecanique 332 (2004). |
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Keywords: | Computational fluid mechanics Hypersonic flow Boundary layer Shock layer Stability Simulation Mécanique des fluides numérique Flux hypersonique Couche limite Couche de choc Stabilité Simulations |
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