Fluid-structure interaction study of the start-up of a rocket engine nozzle
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Publication:435680
DOI10.1016/j.compfluid.2010.03.005zbMath1242.76098OpenAlexW1981381368WikidataQ106518222 ScholiaQ106518222MaRDI QIDQ435680
Luciano Garelli, Rodrigo R. Paz, Mario Alberto Storti
Publication date: 11 July 2012
Published in: Computers and Fluids (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1016/j.compfluid.2010.03.005
Fluid-solid interactions (including aero- and hydro-elasticity, porosity, etc.) (74F10) Shock waves and blast waves in fluid mechanics (76L05) Parallel numerical computation (65Y05) Supersonic flows (76J20)
Related Items (7)
On fluid-shell coupling using an arbitrary Lagrangian-eulerian fluid solver coupled to a positional Lagrangian shell solver ⋮ Application of a partitioned field approach to transient aerothermal problems in rocket nozzles ⋮ Frequency dependency of side loads resulting from shock motion in a forced oscillating rocket nozzle ⋮ Evaluation of a coupling interface for solving fluid-structure interaction problems ⋮ An embedded strategy for the analysis of fluid structure interaction problems ⋮ Adaptive reduced-order modeling for non-linear fluid-structure interaction ⋮ A cut-cell finite volume - finite element coupling approach for fluid-structure interaction in compressible flow
Uses Software
Cites Work
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