Pages that link to "Item:Q435680"
From MaRDI portal
The following pages link to Fluid-structure interaction study of the start-up of a rocket engine nozzle (Q435680):
Displaying 15 items.
- Frequency dependency of side loads resulting from shock motion in a forced oscillating rocket nozzle (Q365484) (← links)
- Starting of an axisymmetric convergent-divergent nozzle in a hypersonic flow (Q477244) (← links)
- A cut-cell finite volume - finite element coupling approach for fluid-structure interaction in compressible flow (Q729430) (← links)
- On fluid-shell coupling using an arbitrary Lagrangian-eulerian fluid solver coupled to a positional Lagrangian shell solver (Q1629761) (← links)
- Application of a partitioned field approach to transient aerothermal problems in rocket nozzles (Q1643695) (← links)
- Evaluation of a coupling interface for solving fluid-structure interaction problems (Q1671549) (← links)
- Adaptive reduced-order modeling for non-linear fluid-structure interaction (Q2245521) (← links)
- An embedded strategy for the analysis of fluid structure interaction problems (Q2414618) (← links)
- Effect of the fluid–structure interaction on solid rocket motors instabilities (Q2831772) (← links)
- (Q4441677) (← links)
- Performance prediction and optimization for liquid rocket engine nozzle (Q4929537) (← links)
- Fluid-structural interaction with application to rocket engines (Q4935647) (← links)
- Starting flow through nozzles with temporally variable exit diameter (Q5695806) (← links)
- Une méthodologie générale pour l’étude numérique du couplage fluide-structure par une approche multicode (Q5755059) (← links)
- A monolithic arbitrary Lagrangian-Eulerian-based finite element strategy for fluid-structure interaction problems involving a compressible fluid (Q6553994) (← links)
