Parameterization dynamics visual design platform for missile launching system

Author:

Yang Haigen1ORCID,Fu Xiao1,Zhan Zhihuan2,Xin Weigang3

Affiliation:

1. Engineering Research Center of Wider and Wireless Communication Technology, Ministry of Education, Nanjing University of Posts and Telecommunications, Nanjing, P.R. China

2. Beijing Electro-Mechanical Engineering Institute, Beijing, P.R. China

3. China International Engineering Consulting Corporation, Beijing, P.R. China

Funder

Chinese Defense Advance Research Program of Science and Technology

the Basic Scientific Research of National Defense

the Open Program of National Engineering Laboratory for Modeling and Emulation in E-Government

Publisher

SAGE Publications

Subject

Mechanical Engineering

Cited by 7 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Research on visual simulation for complex weapon equipment interoperability based on MBSE;Multimedia Tools and Applications;2023-07-06

2. Semianalytical Model for Dynamic Analysis of Missile Vertical Cold Launch;Journal of Spacecraft and Rockets;2022-11

3. A new simplified fluid dynamic model for digital twins of electrohydraulic servovalves;Aircraft Engineering and Aerospace Technology;2021-07-13

4. Influence of pre-stage cavitation on performance of double-nozzle flapper pressure servo valves;Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science;2021-05-23

5. Cavitation suppression in the nozzle-flapper valves of the aircraft hydraulic system using triangular nozzle exits;Aerospace Science and Technology;2021-05

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