Linear stability analysis of hypersonic boundary layers computed by a kinetic approach: a semi-infinite flat plate at $\varvec{4.5\le \mathrm{M}_\infty \le 9}$

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Abstract
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Funding Information
  • Office of Naval Research Global (N00014-1-20-2195)
  • Office of Naval Research Global (N00014-1-20-2195)

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