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- W2625653246 abstract "JAXA have studied the multidisciplinary optimal design method for the next generation rocket turbopump. The concept of the design share information of each component of the rocket turbopump. It will find optimal solution of rotor system in terms of vibrational characteristics. To obtain reliable solution (robustness) of rocket turbopump, the design process should be appropriate. By utilizing axiomatic design theory as a tool of logical design process, we evaluate the current design process for the axial vibrational characteristics. As a results, current design process is appropriate." @default.
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- W2625653246 date "2016-01-01" @default.
- W2625653246 modified "2023-09-26" @default.
- W2625653246 title "Multidisciplinary optimal design of Rocket Turbopump utilized by Axiomatic Design" @default.
- W2625653246 doi "https://doi.org/10.1299/jsmemecj.2016.j1030305" @default.
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