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- W2109696541 abstract "Optimal disturbances for the supersonic ∞ow past a sharp cone are computed in order to assess the efiects due to ∞ow divergence. This geometry is chosen because previously published studies on compressible optimal perturbations for ∞at plate and sphere did not allow to discriminate the in∞uence of divergence alone, as many factors characterized the growth of disturbances on the sphere (∞ow divergence, centrifugal forces and dependence of the edge parameters on the local Mach number). Flow-divergence efiects result in the presence of an optimal distance from the cone tip for which the optimal gain is the largest possible, showing that divergence efiects are stronger in the proximity of the cone tip. By properly rescaling the gain, wavenumber and streamwise coordinate due to the fact that the boundary layer on the sharp cone is p 3 thinner than the one over the ∞at plate, it is found that both the gain and the wavenumber compare fairly well. Moreover, results for the sharp cone collapse into those for the ∞at plate when the initial location for the computation tends to the flnal one and when the azimuthal wavenumber is very large. Results show also that a cold wall enhances transient growth." @default.
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- W2109696541 date "2007-02-01" @default.
- W2109696541 modified "2023-10-16" @default.
- W2109696541 title "Optimal Disturbances in the Supersonic Boundary Layer Past a Sharp Cone" @default.
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- W2109696541 doi "https://doi.org/10.2514/1.22541" @default.
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