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机译:带有不同喷油嘴和喷嘴的脉冲爆震火箭发动机的实验研究
School of Power and Energy, Northwestern Polytechnical University, Xi'an, 710072, PR China;
School of Power and Energy, Northwestern Polytechnical University, Xi'an, 710072, PR China;
School of Power and Energy, Northwestern Polytechnical University, Xi'an, 710072, PR China;
School of Power and Energy, Northwestern Polytechnical University, Xi'an, 710072, PR China;
School of Power and Energy, Northwestern Polytechnical University, Xi'an, 710072, PR China;
detonation; pulse detonation rocket engine; injector; bell-shaped nozzle;
机译:钟形喷嘴对两相脉冲爆震火箭发动机性能影响的实验研究
机译:射流脉冲爆震火箭发动机推进性能的实验研究。
机译:脉冲爆震火箭发动机喷射器内爆震起爆的初步实验研究
机译:喷射流脉冲爆震火箭发动机性能的实验研究
机译:使用无毒超高分子量推进剂的无阀脉冲爆震火箭发动机的实验研究。
机译:柴油发动机喷射器喷嘴喷射特性的分析用剩余燃料油燃料
机译:同轴旋转阀的多循环单管脉冲爆震火箭发动机的实验研究
机译:喷射燃料脉冲爆轰火箭发动机的爆轰起爆