Visualization of the Liquid Layer Combustion of Paraffin Fuel for Hybrid Rocket Applications-Reference-Cited by-同舟云学术

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Visualization of the Liquid Layer Combustion of Paraffin Fuel for Hybrid Rocket Applications

Published:2012-07-30 Issue: Volume: Page:
ISSN:
Container-title:48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
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Author:

Chandler Ashley,Jens Elizabeth,Cantwell Brian,Hubbard G Scott

Publisher

American Institute of Aeronautics and Astronautics

Reference9 articles.

1. Karabeyoglu,M.A.,Cantwell,B.J.,andAltman,D.DevelopmentandTestingofParaffin-BasedHybrid Rocket fuels. AIAA 2001-4503. 37th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit July 8-11,2001/SaltLake City, Utah.

Cited by 37 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 grain length on GOx-paraffin hybrid rocket engines performance and regression rate;International Journal of Heat and Mass Transfer;2024-03

2. Numerical study of the effect of fuel droplets on the combustion proceeding under typical conditions of hybrid rocket engines;Thermophysics and Aeromechanics;2023-06-05

3. Investigation of dynamic mixing combustion characteristics in variable thrust hybrid rocket motors;Combustion and Flame;2023-04

4. Droplet entrainment and its role in the combustion of HTPB/paraffin fuels;Acta Astronautica;2023-03

5. Laser Ignition of Hybrid Rocket Motors: Ignition Characterization and Ignition Mechanism Analysis;AIAA SCITECH 2023 Forum;2023-01-19

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