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Two-phase flow effects on hybrid combustion

Published:1976-03 Issue:3-4 Volume:3 Page:241-263
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Gany A.,Manheimer-Timnat Y.,Wolfshtein M.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference23 articles.

1. Application of steady-state spray equations to combustion modeling;Bracco;AIAA J.,1974

2. Theoretical investigation of hybrid rocket motor employing liquid oxidizer;Gany,1975

3. Parametric study of a hybrid rocket motor;Gany;Israel J. Techn.,1972

4. Study of the influence of oxidizer droplet characteristics on hybrid combustion;Gany;Israel J. Techn.,1975

5. Study of the combustion process in hybrid propulsion;Helman,1972

Cited by 19 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. Hybrid rocket combustion with prevaporized zone;Aircraft Engineering and Aerospace Technology;2013-08-30

2. Micro and Full-Scale Experiments on Hybrid Rocket Fuel and Prelude to Hybrid Rocket Combustor Simulations;49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference;2013-07-12

3. Hybrid Rocket Technology;Defence Science Journal;2011-04-27

4. Population balance modelling of polydispersed particles in reactive flows;Progress in Energy and Combustion Science;2010-08

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

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