An iterative approach for modal analysis of solid rocket motor incorporating frequency dependent modulus
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An iterative approach for modal analysis of solid rocket motor incorporating frequency dependent modulus
An iterative approach for modal analysis of solid rocket motor incorporating frequency dependent modulus
航空动力学报2013年28卷第2期
作者机构:
School of Astronautics, Beijing University of Aeronautics and Astronautics,Beijing,China,100191
作者简介:
基金信息:
DOI:
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纸质出版:2013
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Muhamm adAdnan, SUN Bing, ZHANG Jian-wei, 等. An iterative approach for modal analysis of solid rocket motor incorporating frequency dependent modulus[J]. 航空动力学报, 2013,28(2).
Muhammad Adnan, SUN Bing, ZHANG Jian-wei, et al. An iterative approach for modal analysis of solid rocket motor incorporating frequency dependent modulus[J]. 2013, 28(2).
Muhamm adAdnan, SUN Bing, ZHANG Jian-wei, 等. An iterative approach for modal analysis of solid rocket motor incorporating frequency dependent modulus[J]. 航空动力学报, 2013,28(2).DOI:
Muhammad Adnan, SUN Bing, ZHANG Jian-wei, et al. An iterative approach for modal analysis of solid rocket motor incorporating frequency dependent modulus[J]. 2013, 28(2).DOI:
An iterative approach for modal analysis of solid rocket motor incorporating frequency dependent modulus
The modulus of viscoelastic materials varies with excitation frequency.However
during modal analysis of frequency dependent materials
a material evaluation frequency is necessary because stiffness cannot be modified during eigenfrequency procedure.As a result
only those vibration modes are accurate
of which eigenfrequency is close to the material evaluation frequency.In order to obtain vibration modes of solid rocket motor (SRM) using material modulus based on frequency which is the same as the eigenfrequency
an iterative approach was proposed.Results of the iterative technique show that frequency modes obtained from the method are in complete agreement with the eigenfrequency and material evaluation frequency.
Abstract
The modulus of viscoelastic materials varies with excitation frequency.However
during modal analysis of frequency dependent materials
a material evaluation frequency is necessary because stiffness cannot be modified during eigenfrequency procedure.As a result
only those vibration modes are accurate
of which eigenfrequency is close to the material evaluation frequency.In order to obtain vibration modes of solid rocket motor (SRM) using material modulus based on frequency which is the same as the eigenfrequency
an iterative approach was proposed.Results of the iterative technique show that frequency modes obtained from the method are in complete agreement with the eigenfrequency and material evaluation frequency.