Investigation of Nozzle Stability for the First Ovalization Mode by Numerical Solution of the Fluid Structure Interaction Problem

Details Investigation of Nozzle Stability for the First Ovalization Mode by Numerical Solution of the Fluid Structure Interaction Problem Investigation of Nozzle Stability for the First Ovalization Mode by Numerical Solution of the Fluid Structure Interaction Problem

Feb 2005

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2005esasp.563..331s&link_type=abstract

Proceedings of the Fifth European Symposium on Aerothermodynamics for Space Vehicles (ESA SP-563). 8-11 November 2004, Cologne,

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Scientific paper

The present paper validates results from numerical simulations for side
load generation in rocket nozzles against related data from analytical
models that are presently used for rocket engine nozzle design
activities. Key words: Nozzle stability; nozzle ovalization; flow
structure interaction.

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