Dual Base Swirl Injector Design for Increasing Specific Impluse in a Liquid-Fuel Rocket Engine
Optimized injectors spray and consequently their proper fluid distribution is one of the most important factors determining the thrust force and combustion stability. Reaching a stable combustion with a high specific impulse needs a proper fuel distribution and atomization. Asymmetric distribution o...
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| 主要な著者: | , , |
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| フォーマット: | Artigo |
| 言語: | Persa |
| 出版事項: |
Aerospace Research Institute
2009-03-01
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| シリーズ: | فصلنامه علوم و فناوری فضایی |
| 主題: | |
| オンライン･アクセス: | https://jsst.ias.ir/article_14377_9cd138c0e06fd1fe7a5882ae8a573902.pdf |
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