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- W2350222375 abstract "Supersonic anti-ship missile fuze-warhead system was wholly researched.Modal analysis of fuze and warhead system was simulated by ANSYS,the first order 20 inherent frequency and the frequency response function of ignition control circuit flame-proof rotor,booster,expansion booster and warhead shell by means of harmonic response analysis with sine excitation unit along the axis direction were obtained.By analyzing the frequency response function,the resonance frequency corresponding to the biggest displacement response of fuzewarhead system was obtained,and comparing the major parts of fuze-warhead system with the displacement response of warhead shell,it was concluded that the displacement response of detonating tube,booster tube,expansion of detonation tube were greater than that of warhead shell,while the displacement response of ignition control circuit and flame-proof rotor were less than that of warhead shell.The analysis indicated that,in order to depress the influence of overload along axis direction on the ignition control circuit,the overload on the warhead shell should be depressed,and flame-proof rotor and igniter train,could be taken into consideration during structural design." @default.
- W2350222375 created "2016-06-24" @default.
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- W2350222375 date "2015-01-01" @default.
- W2350222375 modified "2023-09-27" @default.
- W2350222375 title "Frequency Response Characteristics of the Supersonic Anti-ship Missile Fuze-warhead System" @default.
- W2350222375 hasPublicationYear "2015" @default.
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