对在高焓、持续工作时间短暂设备中进行伴有燃烧过程的气体动力模型的试验方法的特点作了介绍。根据俄罗斯科学院西伯利亚分院理论及应用研究所组织这种试验工作所积累的经验 ,描述了解决各种各类与燃烧有关的问题的模型配备 ;在发动机进气道中的推力空气动力特性、压力及热通量的测量结果等等。由此说明试验时间为 50～ 2 0 0ms的热射式风洞是解决燃烧问题的可靠设备 The characteristics of the experimental method of gas dynamic model with combustion process in high-enthalpy, short-duration equipment are described. Based on the experience accumulated by the Siberian branch of the Institute of Theoretical and Applied Sciences of the Russian Academy of Sciences in organizing such experimental work, model configurations for solving various types of combustion-related problems are described; thrust aerodynamic characteristics, pressure and heat in the intake of the engine Flux measurement results and more. This shows that the test time of 50 ~ 2 0 thermal spray wind tunnel is to solve the problem of burning a reliable device