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固体火箭发动机振型计算和实验研究
引用本文:邹俊伟 孙维申. 固体火箭发动机振型计算和实验研究[J]. 兵工学报, 1992, 13(2): 38-45
作者姓名:邹俊伟 孙维申
作者单位:北京理工大学(邹俊伟,孙维申),北京理工大学(邢春景)
摘    要:

关 键 词:固体 火箭发动机 振型计算

CALCULATION OF VIBRATION MODE AND ITS EXPERIMENTAL STUDY IN SOLID ROCKET MOTORS
Zou Junwei Sun Weishen Xing Chunjing. CALCULATION OF VIBRATION MODE AND ITS EXPERIMENTAL STUDY IN SOLID ROCKET MOTORS[J]. Acta Armamentarii, 1992, 13(2): 38-45
Authors:Zou Junwei Sun Weishen Xing Chunjing
Affiliation:Beijing Institute of Technology
Abstract:In this paper, a method for the calculation of vibration mode in rocket motors is presented, and a corresponding program is worked out. Values calculated with this program are consistent with theoretical or experimental results, the results, indicating that the program is soundly based. A new type of vibration excitation apparatus-turbo vibration exciter is also introduced in this paper, used for the determination of natural frequency of acoustic cavities, and of acoustic damping coefficients of motor.
Keywords:solid rocket motor   prediction of combustion stability   vibration mode calculation   instable combustion in solid rocket motors  
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