supported by the National Natural Science Foundation of China (No. 51306153);the Natural Science Foundation of Shanxi Province of China (No. 2010JQ7005);Doctoral Fund of Ministry of Education of China (No. 20116102120027);Northwestern Polytechnical University Foundation for Fundamental Research (No. NPU-FFRJCY20130129)
In order to test the feasibility of a new thrust stand system based on impulse thrust mea- surement method, a liquid-fueled pulse detonation engine (PDE) is designed and built. Thrust per- formance of the engine is ...