Pages that link to "Item:Q1932272"
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The following pages link to Delayed detached eddy simulation of the end-effect regime and side-loads in an overexpanded nozzle flow (Q1932272):
Displaying 7 items.
- Unsteadiness of flow separation and end-effects regime in a thrust-optimized contour rocket nozzle (Q1430081) (← links)
- Time-accurate CFD predictions and data validation for side load generation by flow-structure coupling in over-expanded rocket nozzles (Q1778088) (← links)
- Nozzle flow separation (Q1932269) (← links)
- Unsteadiness in shock-induced separated flow with subsequent reattachment of supersonic annular jet (Q2446538) (← links)
- Compressibility effects on the vortical flow over a 65° sweep delta wing (Q3557461) (← 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)