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A Kinetic Study of Hypersonic Boundary Layer Second Mack Mode Instabilities
A flat-plate laminar boundary layer is simulated at a free stream Mach number of 6 and unit Reynolds number $Re_1 \sim 1.18\times 10^7$ m$^{-1}$ using the Direct Simulation Monte Carlo (DSMC) method to capture and analyze spontaneous second-mode instability growth. Power spectral density (PSD) analy
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