Two-Phase Vorticoacoustic Flow Interactions in Solid-Propellant Rocket Motors
β Scribed by Cai, Weidong; Ma, Fuhua; Yang, Vigor
- Book ID
- 121531828
- Publisher
- American Institute of Aeronautics and Astronautics
- Year
- 2003
- Tongue
- English
- Weight
- 451 KB
- Volume
- 19
- Category
- Article
- ISSN
- 0748-4658
- DOI
- 10.2514/2.6142
No coin nor oath required. For personal study only.
π SIMILAR VOLUMES
Segmentation of solid propellant rocket motors has been demonstrated to be a source of unpredicted and undesirable pressure and thrust oscillations. Surface discontinuities are the primary cause of these vortex-sheddingdriven oscillations, which result from a strong coupling between the shear layer
The present work is devoted to the numerical simulation of two important phenomena in the field of solid propellant rocket motors: the first is acoustic boundary layers that develop above the burning propellant; the other is a periodic vortex-shedding phenomenon which is the result of a strong coupl
This volume is the proceedings of the Fifth International Conference on Fluid Mechanics (ICFM-V), the primary forum for the presentation of technological advances and research results in the fields of theoretical, experimental, and computational Fluid Mechanics. Topics include: flow instability and