3D turbulent Navier Stokes simulations of ignition transients in solid rocket motors
Author:
Affiliation:
1. SEP, St.-Medard-en-Jalles, France
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1998-3843
Reference1 articles.
Cited by 4 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. A new simulation strategy for solid rocket motor ignition: coupling a CFD code with a one-dimensional boundary flame model, verification against a fully resolved approach;AIAA Propulsion and Energy 2021 Forum;2021-07-28
2. Parametric Study on Solid Rocket Motor Ignition Transient and Pressure Oscillations Onset;Journal of Propulsion and Power;2015-07
3. 3-D Simulations of Ignition Transients in the RSRM;41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2005-07-10
4. Recent Progress In SRM Ignition Transient Modeling;39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit;2003-06-26
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