Data for: Heat Transfer Characteristic Analysis of a Novel Annular Nuclear Heat Exchanger for Propulsion System
The model in this paper is an engine model with MA<1. In order to study the air heating and flow process in the combustion chamber, the model is simplified. A one-dimensional adiabatic flow model is used to simplify the engine intake and exhaust processes. A steady one-dimensional heating model is used to simplify the combustion and heating process of the combustion chamber. At present, these simplifications accord with the general rule of flow heat transfer in engine and have been widely used in numerical simulation.