The study of one-dimensional flow analysis model of the combustor in supersonic combustion experiments

The existent one-dimensional flow analysis models for supersonic combustor were studied. The results showed that the complete solution of one-dimensional combustion flow field could only be obtained with either necessary experimental data or some empirical methods. With the improved model, the uncertainty in the process of data reduction could be reduced. The adaptability of the code could be enhanced. The calculated values of static and stagnation pressure showed good agreement with experimental data.