Using data collected in a NASA wind tunnel, researchers replicated the hypersonic flow conditions of a compression ramp flow using Direct Numerical Simulation. Using data collected in a NASA Langley ...
Understanding the boundary layer transition and the influence of surface roughness in hypersonic flows is critical for advancing aerospace design and safety. At these extreme speeds, the interplay ...
Hypersonic boundary layer dynamics and stability form a critical research area with implications for the design and operation of high-speed aerospace vehicles. At speeds exceeding Mach 5, the ...
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