共 50 条
- [1] EXPERIMENTAL INVESTIGATION OF THRUST AUGMENTATION BY EJECTORS ON A PULSE DETONATION ENGINE THERMAL SCIENCE, 2015, 19 (06): : 2105 - 2114
- [2] Experimental investigation on net thrust characteristics of pulse detonation engine Nanjing Hangkong Hangtian Daxue Xuebao/Journal of Nanjing University of Aeronautics and Astronautics, 2004, 36 (03): : 273 - 277
- [3] Investigation on common nozzle of triple-tube pulse detonation engine with kerosene/air Hangkong Dongli Xuebao/Journal of Aerospace Power, 2008, 23 (05): : 840 - 844
- [4] Experimental investigation on a kerosene/air air-breathing pulse detonation engine Shiyan Liuti Lixue/Journal of Experiments in Fluid Mechanics, 2009, 23 (03): : 35 - 39
- [5] Experimental investigation on small-scale pulse detonation engine with kerosene/air Hangkong Xuebao, 2009, 11 (2015-2022): : 2015 - 2022
- [7] Detonation characteristic on kerosene/oxygen pulse detonation rocket engine Kung Cheng Je Wu Li Hsueh Pao, 2008, 1 (168-170):
- [8] Experimental investigation on a six-tube air-breathing pulse detonation engine Hangkong Dongli Xuebao/Journal of Aerospace Power, 2011, 26 (09): : 1981 - 1985
- [9] Experiment on heat exchange and cooling of pulse detonation engine detonation tube wall Hangkong Dongli Xuebao/Journal of Aerospace Power, 2014, 29 (12): : 2817 - 2823