| 多孔超高燃速推进剂的燃烧理论 |
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| 引用本文： | 杨荣杰.多孔超高燃速推进剂的燃烧理论[J].固体火箭技术,1993(1):30-34. |
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| 作者姓名： | 杨荣杰 |
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| 作者单位： | 北京理工大学 北京100081 |
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| 摘 要： | 概述了有关多孔透气性超高燃速推进剂的代表性燃烧理论,其包括对流燃烧理论、两相流燃烧理论和非均一燃烧理论,介绍了它们的基本观点和主要结果,指出了彼此间的差异。
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| 关 键 词： | 火箭推进剂 推进剂 燃烧波 |
Combustion Theories of Porous Solid Propellants of Ultra-high Burn Rate |
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| Yang Rongjie Beijing Institute of Technology,Beijing.Combustion Theories of Porous Solid Propellants of Ultra-high Burn Rate[J].Journal of Solid Rocket Technology,1993(1):30-34. |
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| Authors: | Yang Rongjie Beijing Institute of Technology Beijing |
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| Institution: | Yang Rongjie Beijing Institute of Technology,Beijing,100081 |
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| Abstract: | Representative combustion theories of porous permeable propellants of ultra-high burn rate were generalized.They are the convective combustion theory,the two phase flow combustion theory and the inhomogeneous combustion theory.Main viewpoints and results of the theories were introduced. |
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| Keywords: | Solid rocket propellant Propellant combustion Burn wave Burn rate |
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