Simulation Study on the Thermodynamics System of Aircraft Avionics Pod
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Simulation model of the thermodynamics system of aircraft avionics pod was established and its dynamic characteristics of thermal load and main temperature parameters during the whole flying were obtained, which assisted in the selection and verification of the refrigeration system. In addition, a valid proposal about the optimization of the hull framework was offered. The study proved that dynamic simulation is an advanced calculation and analysis method for the design and model selection of the refrigeration system.