Pages that link to "Item:Q2891627"
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The following pages link to Dynamic effects on the transition between two-dimensional regular and Mach reflection of shock waves in an ideal, steady supersonic free stream (Q2891627):
Displaying 16 items.
- A study of shock wave interaction with a rotating cylinder (Q706388) (← links)
- The non-stationary hysteresis phenomenon in shock wave reflections (Q2878378) (← links)
- Time history of regular to Mach reflection transition in steady supersonic flow (Q2891833) (← links)
- Unsteady Navier-Stokes simulations of regular-to-Mach reflection transition on an ideal surface (Q3395861) (← links)
- Shock-wave/expansion-wave interactions and the transition between regular and Mach reflection (Q3432894) (← links)
- A Theory for Spontaneous Mach-Stem Formation in Reacting Shock Fronts. II. Steady-Wave Bifurcations and the Evidence for Breakdown (Q3707667) (← links)
- Steady Mach reflection with two incident shock waves (Q4559134) (← links)
- Three-dimensional shock wave reflection transition in steady flow (Q4559296) (← links)
- Unsteady effects of strong shock-wave/boundary-layer interaction at high Reynolds number (Q4594073) (← links)
- Numerical and experimental investigation of oblique shock wave reflection off a water wedge (Q4972280) (← links)
- A study on the RR-to-MR transition of shock wave reflections near the leading edge in hypersonic flows (Q4997909) (← links)
- Similarity in Mach stem evolution and termination in unsteady shock-wave reflection (Q5121248) (← links)
- Viscous jetting and Mach stem bifurcation in shock reflections: experiments and simulations (Q5144757) (← links)
- Transition study for asymmetric reflection between moving incident shock waves (Q5160158) (← links)
- On regular reflection to Mach reflection transition in inviscid flow for shock reflection on a convex or straight wedge (Q5207621) (← links)
- Dynamics of unsteady asymmetric shock interactions (Q5217662) (← links)
