Pages that link to "Item:Q1662877"
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The following pages link to Modeling of supersonic/hypersonic boundary layer transition using a single-point approach (Q1662877):
Displaying 5 items.
- A Favré averaged transition prediction model for hypersonic flows (Q617245) (← links)
- Development of an intermittency equation for the modeling of the supersonic/hypersonic boundary layer flow transition (Q647472) (← links)
- Convergence acceleration for high-order shock-fitting methods in hypersonic flow applications with efficient implicit time-stepping schemes (Q2019962) (← links)
- An improved physics-informed transition-turbulence model for asymmetric transition over supersonic rotating projectiles (Q2129536) (← links)
- Amplification factor transport transition model for high-speed flows (Q6095966) (← links)