机译:基于多层夹心模型的非稳态火箭电机中AP / HTPB复合推进剂的火焰动态
Northwestern Polytech Univ Internal Flow & Thermal Struct Lab Sci & Technol Combust Xian 710072 Shaanxi Peoples R China;
Northwestern Polytech Univ Internal Flow & Thermal Struct Lab Sci & Technol Combust Xian 710072 Shaanxi Peoples R China;
Northwestern Polytech Univ Internal Flow & Thermal Struct Lab Sci & Technol Combust Xian 710072 Shaanxi Peoples R China;
Northwestern Polytech Univ Internal Flow & Thermal Struct Lab Sci & Technol Combust Xian 710072 Shaanxi Peoples R China;
Ammonium perchlorate; hydroxyl-terminated polybutadiene (AP; HTPB) composite propellant; Oscillation; Sandwich model; Solid rocket motor;
机译:基于多层夹心模型的非定常火箭发动机中AP / HTPB复合推进剂的火焰动力学
机译:基于三明治模型的AP / HTPB推进剂火焰火焰描述功能的理论研究
机译:火箭发动机环境中Ap / htpb复合推进剂燃烧的模型
机译:AP / HTPB基复合推进剂数学模型的燃烧速率与实验结果的比较
机译:AP / HTPB复合推进剂在具有声振荡的火箭发动机中的两相流相互作用和燃烧。
机译:冲击载荷下HTPB推进剂的动态机械响应及损伤机制
机译:Dekomposisi Termal Propelan Komposit Berbasis alynium perklorat /羟基封端的聚丁二烯(AP / HTPB)(高氯酸铵/羟基化合物聚丁二烯(AP / HTPB)复合固体推进剂的热分解分析)
机译:Vidhaeftning foer en HTpB-Baserad Kompositkrutisolering mot Nagra moderna Rakethylsmaterial(基于HTpB的复合推进剂衬里与现代火箭发动机外壳材料的粘合)