为了使试验结果尽可能接近真实燃烧过程，本文提出一种适用于非等温射流的后移燃烧器几何相似模型。
In order to approach as near as possible the actual combustion process, a mode! With geometric similarities for moved-out burner is described which is applicable to non-isothermal jet.
本文是以燃烧过程的动力机理和燃烧系统的相似理论为基础，结合发动机的几种典型燃烧情况来研究低速燃烧系统稳态工况的模化法则。
Based on similarity Principles and some typical operating mechanisms of combustion engines, the present paper suggests the modeling rules of steady performances of combustors at low flow Mach number.
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