Pages that link to "Item:Q1430081"
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The following pages link to Unsteadiness of flow separation and end-effects regime in a thrust-optimized contour rocket nozzle (Q1430081):
Displaying 13 items.
- Scale analysis and experimental observations of shock-induced turbulent boundary layer separation in nozzles (Q885959) (← links)
- Unsteady separated two-throat nozzle flows (Q1430092) (← links)
- Nozzle flow separation (Q1932269) (← links)
- Delayed detached eddy simulation of the end-effect regime and side-loads in an overexpanded nozzle flow (Q1932272) (← links)
- Transient three-dimensional startup side load analysis of a regeneratively cooled nozzle (Q1932273) (← links)
- Shock wave boundary layer interaction (Q1932298) (← links)
- Convergent-divergent nozzle under highly overexpanded conditions (Q2388172) (← links)
- Unsteadiness in shock-induced separated flow with subsequent reattachment of supersonic annular jet (Q2446538) (← links)
- Numerical study of the start-up process in an optimized rocket nozzle (Q2853524) (← links)
- Stochastic rocket dynamics under random nozzle side loads: Ornstein-Uhlenbeck boundary layer separation and its coarse grained connection to side loading and rocket response (Q3015376) (← links)
- (Q4441677) (← links)
- Jet resonance in truncated ideally contoured nozzles (Q4997901) (← links)
- Flow dynamics and wall-pressure signatures in a high-Reynolds-number overexpanded nozzle with free shock separation (Q5113240) (← links)