Theoretical investigation of hybrid rocket combustion by numerical methods-Reference-Cited by-同舟云学术

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Theoretical investigation of hybrid rocket combustion by numerical methods

Published:1974-04 Issue:2 Volume:22 Page:171-190
ISSN:0010-2180
Container-title:Combustion and Flame
language:en
Short-container-title:Combustion and Flame

Author:

Helman D.,Wolfshtein M.,Manheimer-Timnat Y.

Publisher

Elsevier BV

Subject

General Physics and Astronomy,Energy Engineering and Power Technology,Fuel Technology,General Chemical Engineering,General Chemistry

Reference19 articles.

1. Ninth Symposium (International) on Combustion;Marxman,1963

2. Tenth Symposium (International) on Combustion;Marxman,1965

3. Internal ballistic considerations in hybrid rocket design.

4. Twelfth Symposium (International) on Combustion;Marxman,1969

Cited by 14 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

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3. Development and Validation of a 1.5-D Combustion Chamber Model for a Hybrid Rocket Engine Applied to a Cylindrical HDPE Chamber;AIAA Propulsion and Energy 2021 Forum;2021-07-28

4. Two-phase flow effect on hybrid rocket combustion;Acta Astronautica;2009-10

5. A physics based mathematical model to predict the regression rate in an ablating hybrid rocket solid fuel;37th Joint Propulsion Conference and Exhibit;2001-07-08

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