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Attitude simulation of launch process of vehicular missile
Yu Jun Chen
*
,
Yi Jiang
*
Corresponding author for this work
School of Aerospace Engineering
Beijing Institute of Technology
Research output
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Article
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peer-review
3
Citations (Scopus)
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Engineering
Dynamic Models
100%
Flexible Couplings
100%
Experimental Result
50%
Computer Simulation
50%
Simulation Result
50%
Dynamic Response
50%
Impact Force
50%
Characteristic Vibration
50%
Physics
Dynamic Response
100%
Jet Flow
100%