By means of analysis of the trailing flow field structure of different circle injectors
the relationship between the position of shock wave specific to injector diameter
and the pressure of inlet flow/pressure of environment was determined.From numerical simulation of circle injector with cylinder resonance tube and cone resonance tube
it is concluded that the necessary condition the intense resonance can occur within resonance tube lies in the position of resonance tube's entrance in the expand wave field;and if the position is in shock wave field
the resonance can not occur within resonance tube.Now the region where resonance occurs can be gained from free jet flow field by means of numerical simulation.The best matching between injector and resonance tube was obtained by analyzing the resonance heating performance variation with different diameter injectors.
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Related Author
FU Qing-fei
YANG Li-jun
QU Yuan-yuan
GU Bin
Ping ZHANG
Shan LU
Xin JING
Mao YANG
Related Institution
School of Astronautics, Beijing University of Aeronautics and Astronautics
School of Power and Energy,Northwestern Polytechnical University
Nondestructive Testing and Evaluation Laboratory, Dalian University of Technology
College of Civil Engineering, Hefei University of Technology
Key Laboratory of Aerospace Chemical Power Technology, Hubei Institute of Aerospace Chemical Techologh, China Aerospace Science and Technology Corporation,Xiangyang Hubei