Pages that link to "Item:Q2891833"
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The following pages link to Time history of regular to Mach reflection transition in steady supersonic flow (Q2891833):
Displaying 9 items.
- Numerical investigations of transition between regular and Mach reflections caused by free-stream disturbances (Q1864482) (← links)
- Transition between the regular and Mach shock interaction regimes initiated by a temperature disturbance (Q1936900) (← links)
- Shock reflection in the presence of an upstream expansion wave and a downstream shock wave (Q2878475) (← links)
- Dynamic effects on the transition between two-dimensional regular and Mach reflection of shock waves in an ideal, steady supersonic free stream (Q2891627) (← links)
- Steady Mach reflection with two incident shock waves (Q4559134) (← links)
- Shock transformation and hysteresis in underexpanded confined jets (Q4594068) (← links)
- Prediction of Mach stem height in compressible open jets. Part 1. Overexpanded jets (Q5080977) (← links)
- Transition study for asymmetric reflection between moving incident shock waves (Q5160158) (← links)
- Reflection and transition of planar curved shock waves (Q5884292) (← links)