Abstract
Muzzle vibration is one of the most important factors influencing the firing dispersion of gun. In order to study the technical approaches to reducing the muzzle vibration, a launch dynamic model of a large caliber gun is established based on the nonlinear finite element theory, in which the contact impact between interacting components is considered. The influences of different fixed forms and different locations of the counter-recoil mechanism and recoil mechanism on muzzle vibration are studied by numerical computation, and the load transfer rules of the guns with different structural arrangements are analyzed. The optimal structural arrangement is determined by contrastively analyzing the muzzle vibration responses. The results can provide theoretical reference to the overall structure design of the gun systems.
Original language | English |
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Pages (from-to) | 1209-1214 |
Number of pages | 6 |
Journal | Binggong Xuebao/Acta Armamentarii |
Volume | 34 |
Issue number | 10 |
DOIs | |
Publication status | Published - Oct 2013 |
Externally published | Yes |
Keywords
- Contact impact
- Load transfer rule
- Muzzle vibration
- Nonlinear finite element
- Ordnance science and technology