Simulations of Solid-Propellant Rockets: Effects of Aluminum Droplet Size Distribution
Author:
Affiliation:
1. University of Illinois at Urbana–Champaign, Urbana, Illinois 61801
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.17326
Reference42 articles.
1. Fluid flow in regions bounded by porous surfaces
2. An example of steady laminar flow at large Reynolds number
3. Rotational axisymmetric mean flow and damping of acoustic waves in asolid propellant rocket.
4. Improvements to the Solid Performance Program (SPP)
Cited by 58 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. Study on the dynamic numerical simulation of flow and combustion in hybrid rocket motors based on a discrete phase model;Acta Astronautica;2024-02
2. Multiphase Effects on Solid Rocket Nozzle Performance;Journal of Propulsion and Power;2023-11
3. Modeling of aluminum agglomeration at solid propellant burning surface by combining aluminum ignition with LDP-SC cluster analysis;Combustion and Flame;2023-10
4. Investigation on burning behaviors of aluminum agglomerates in solid rocket motor with detailed combustion model;Acta Astronautica;2023-05
5. A particle resolved simulation approach for studying shock interactions with moving, colliding solid particles;Computers & Fluids;2022-11
1.学者识别学者识别
2.学术分析学术分析
3.人才评估人才评估
"同舟云学术"是以全球学者为主线,采集、加工和组织学术论文而形成的新型学术文献查询和分析系统,可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容,当前同舟云学术共收录了国内外主流学术期刊6万余种,收集的期刊论文及会议论文总量共计约1.5亿篇,并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询!咨询电话:010-8811{复制后删除}0370
www.globalauthorid.com
TOP
Copyright © 2019-2024 北京同舟云网络信息技术有限公司 京公网安备11010802033243号 京ICP备18003416号-3