Effect of Fluid/Structure Coupling on Unstable Mechanisms in Solid Rocket Motor
Author:
Affiliation:
1. Instituto Tecnológico de Aeronáutica, 12228-901 São José dos Campos, Brazil
2. Ecole Nationale Supérieure de Mécanique et d’Aérotechnique, 86960 Chasseneuil, France
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.48639
Reference17 articles.
1. Vortex Shedding in a Large Solid Rocket Motor Without Inhibitors at the Segment Interfaces
2. Vortex Shedding Induced Sound Inside a Cold-Flow Simulation of Segmented Chamber
3. On the dependence on the formulation of some nonparallel stability approaches applied to the Taylor flow
4. The generation and evolution of unsteady vorticity in a model of a solid rocket engine chamber
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1. Computing compressible internal flows by means of an Immersed Boundary Method;Computers & Fluids;2014-06
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