Boundary layer combustion of HTPB/paraffin fuels for hybrid propulsion applications
Author:
Funder
National Natural Science Foundation of China
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference30 articles.
1. Transient investigation of nozzle erosion in a long-time working hybrid rocket motor;Tian;Aerosp. Sci. Technol.,2021
2. Computational fluid-dynamic modeling of the internal ballistics of paraffin-fueled hybrid rocket;Martino;Aerosp. Sci. Technol.,2019
3. Regression rate modeling of HTPB/paraffin fuels in hybrid rocket motor;Wang;Aerosp. Sci. Technol.,2022
4. Experimental demonstration of an end-burning swirling flow hybrid rocket engine;Lestrade;Aerosp. Sci. Technol.,2019
5. Combustion performance of a novel hybrid rocket fuel grain with a nested helical structure;Wang;Aerosp. Sci. Technol.,2020
Cited by 11 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. Effect of characteristic structure of nested composite hybrid rocket fuel grain on combustion properties;Acta Astronautica;2024-05
2. Superior Al90Mg10-Based Composite Fuel Grain for a Hybrid Rocket Engine;Journal of Spacecraft and Rockets;2024-04-22
3. A comprehensive fluid–solid coupling dynamic simulation for spatiotemporal distribution of regression rate in hybrid rocket motors;Chinese Journal of Aeronautics;2024-02
4. Droplet entrainment characteristics of HTPB/Paraffin blended fuels for hybrid rocket motors;Acta Astronautica;2024-01
5. Thermal evaluation of MHD boundary‐layer flow of hybridity nanofluid via a 3D sinusoidal cylinder;ZAMM - Journal of Applied Mathematics and Mechanics / Zeitschrift für Angewandte Mathematik und Mechanik;2023-09-06
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