Numerical modeling of perturbation propagation in a supersonic boundary layer
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Abstract
The growth of two-dimensional disturbances generated in a supersonic (M∞ = 6) boundary layer on a flat plate by a periodic perturbation of the injection/suction type is investigated on the basis of a numerical solution of the Navier-Stokes equations. For small initial perturbation amplitudes, the secondmode growth rate obtained from the numerical modeling coincides with the growth rate calculated using linear theory with account for the non-parallelism of the main flow. Calculations performed for large initial perturbation amplitudes reveal the nonlinear dynamics of the perturbation growth downstream, with rapid growth of the higher multiple harmonics.
Keywords
Navier-Stokes equations supersonic flow boundary layer perturbations numerical modelingPreview
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