The method developed in this paper can be used in the research field of the Ducted Rocket and fuel-rich propellant, to reduce the experimental cost effetely and shorten the research period greatly.

• 对于固体冲压发动机和贫氧推进剂的研制来说,本文研究的方法既可有效地降低试验成本,又可大大缩短研制周期,具有一定的工程应用价值。