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- W3119155282 abstract "Laminar to turbulent boundary layer transition is known to be sensitive to freestream disturbances. However, the disturbances in the upper atmosphere are not well characterized, and a multi-university effort to characterize turbulence and particle distributions in the stratosphere aims to address that. This paper considers the numerical methods associated with simulating shock-turbulence interactions for a hypersonic sphere-cone. Atmospheric turbulence is first generally characterized, and then a turbulent shear simulation is characterized in relation to hypersonic flight in order to establish a method for simulating the interaction between hypersonic vehicles and atmospheric turbulence. Low-dissipation Direct Numerical Simulation (DNS) methods for the compressible Navier-Stokes equations are compared with linear equations for planar wave and oblique shock interaction and found to accurately simulate the shock-disturbance interaction. Linear growth of boundary layer waves due to interaction with the second mode instability in hypersonic boundary layer is also simulated with low dissipation DNS and found to compare well with predictions from the Parabolized Stability Equations (PSE). Lastly, atmospheric turbulence in relation to hypersonic flight and simulation requirements to determine it's effect on hypersonic boundary layer transition are discussed." @default.
- W3119155282 created "2021-01-18" @default.
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- W3119155282 date "2021-01-04" @default.
- W3119155282 modified "2023-10-05" @default.
- W3119155282 title "Investigation of Atmospheric Turbulence and Shock Interaction for a Hypersonic Sphere-Cone" @default.
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- W3119155282 doi "https://doi.org/10.2514/6.2021-1325" @default.
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