Pages that link to "Item:Q4997909"
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The following pages link to A study on the RR-to-MR transition of shock wave reflections near the leading edge in hypersonic flows (Q4997909):
Displaying 5 items.
- Dynamic effects on the transition between two-dimensional regular and Mach reflection of shock waves in an ideal, steady supersonic free stream (Q2891627) (← links)
- Transitions of shock interactions on V-shaped blunt leading edges (Q5023218) (← links)
- Theoretical study on regular reflection of shock wave–boundary layer interactions (Q5115445) (← links)
- Supersonic flow fields resulting from axisymmetric internal surface curvature (Q5231553) (← links)
- Geometric criterion for RR↔MR transition in hypersonic double-wedge flows (Q5305006) (← links)