Frequency dependency of side loads resulting from shock motion in a forced oscillating rocket nozzle

DOI10.1016/j.compfluid.2011.06.001zbMath1271.76158OpenAlexW2030910054MaRDI QIDQ365484

Emmanuel Lefrançois

Publication date: 4 September 2013

Published in: Computers and Fluids (Search for Journal in Brave)

Full work available at URL: http://www.sciencedirect.com/science/article/pii/S0045793011001897

zbMATH Keywords

fluid-structure interactionoverexpanded rocket nozzlepiston-analogyrigid body oscillationsside loads

Mathematics Subject Classification ID

Fluid-solid interactions (including aero- and hydro-elasticity, porosity, etc.) (74F10) Finite element methods applied to problems in solid mechanics (74S05) Shock waves and blast waves in fluid mechanics (76L05) Finite element methods applied to problems in fluid mechanics (76M10)

Uses Software

• SHASTA

Cites Work

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• Fluid-structure interaction study of the start-up of a rocket engine nozzle
• Fully multidimensional flux-corrected transport algorithms for fluids
• Weighted essentially non-oscillatory schemes
• On the significance of the geometric conservation law for flow computations on moving meshes
• A numerical investigation of side-loads resulting from rigid body motions of an overexpanded engine nozzle
• Mesh Moving Techniques for Fluid-Structure Interactions With Large Displacements
• A simple mesh deformation technique for fluid-structure interaction based on a submesh approach
• Mixed explicit/implicit time integration of coupled aeroelastic problems: Three‐field formulation, geometric conservation and distributed solution
• Numerical Study of the Aeroelastic Stability of an Overexpanded Rocket Nozzle
• Fluid-structural interaction with application to rocket engines
• Systems of conservation laws
• Numerical validation of a stability model for a flexible over-expanded rocket nozzle
• Flux-corrected transport. I: SHASTA, a fluid transport algorithm that works

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