Pages that link to "Item:Q1932271"
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The following pages link to Shock structure in separated nozzle flows (Q1932271):
Displaying 6 items.
- Experimental and numerical analysis of the structure of pseudo-shock systems in Laval nozzles with parallel side walls (Q633507) (← links)
- Scale analysis and experimental observations of shock-induced turbulent boundary layer separation in nozzles (Q885959) (← links)
- Unsteadiness of flow separation and end-effects regime in a thrust-optimized contour rocket nozzle (Q1430081) (← links)
- Nozzle flow separation (Q1932269) (← links)
- A model to predict the Mach reflection of the separation shock in rocket nozzles (Q3395810) (← links)
- Flow dynamics and wall-pressure signatures in a high-Reynolds-number overexpanded nozzle with free shock separation (Q5113240) (← links)