Of particular importance in the design of hybrid rocket motors is the fuel surface regression rate and the manner in which it varies with operation conditions.
燃面后退速率以及在工作条件改变过程中的变化，对混合发动机的设计有很大的影响。
参考来源 - 固液混合发动机燃烧与燃速特性研究·2,447,543篇论文数据，部分数据来源于NoteExpress
固液混合火箭发动机的燃面后退速率低是制约该类发动机应用的主要因素。
The low fuel regression rate in hybrid motor is the principal factor affecting the application of the motor.
本文首先通过对混合发动机燃烧过程的理论分析，初步建立了混合燃烧模型，并由此得到了燃面后退速率的理论表达式。
The paper summarizes and discusses different types of regression rate models that have been developed by several researchers during previous investigations of hybrid combustion.
应用推荐