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介绍了含铝复合推进剂发动机试验时,对其喷管进行的烧蚀和温度场测量,获得了复合喷管结构中的烧蚀和瞬时温度分布.
This paper introduced the ablation and temperature field measurement of the nozzle of the aluminum-containing composite propellant engine. The ablation and instantaneous temperature distribution in the composite nozzle structure were obtained.