High-order computation of burning propellant surface and simulation of fluid flow in solid rocket chamber-Reference-Cited by-同舟云学术

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High-order computation of burning propellant surface and simulation of fluid flow in solid rocket chamber

Published:2014-07-25 Issue: Volume: Page:
ISSN:
Container-title:50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference
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Author:

Gueyffier Denis,Roux Francois-Xavier,Fabignon Yves,Chaineray Gilles,Lupoglazoff Nicolas,Vuillot Francois,Alauzet Frederic

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2014-3612

Reference41 articles.

1. Analytical Methods for Predicting Grain Regression in Tactical Solid-Rocket Motors

2. Design and Optimization of 3D Radial Slot Grain Configuration

3. ±3-Sigma based design optimization of 3D Finocyl grain

Cited by 3 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. Shape and material optimization of problems with dynamically evolving interfaces applied to solid rocket motors;Structural and Multidisciplinary Optimization;2022-08

2. Solid Rocket Motor Internal Ballistics Simulation Considering Complex 3D Propellant Grain Geometries;Energetic Materials Research, Applications, and New Technologies;2018

3. Simple Surface-Tracking Methods for Grain Burnback Analysis;Journal of Propulsion and Power;2015-09

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