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- W2762795063 abstract "In order to obtain lower heat flux density of stagnation point and higher terminal velocity at the initial stage of hypersonic re-entry warhead, aerodynamic configuration of reentry warhead should be optimized relatively quickly. The overall aerodynamic configuration of reentry warhead were researched. The ballistic model, the pneumatic model and the atmosphere model were built. An approach of aerodynamic parameters optimization was established, taking maximum terminal velocity and minimum heat flux density as optimizing target function. The two methods of aerodynamic characteristics were compared with the engineering algorithm and the panel method. The research results provide a theoretical basis for the shape parameters of reentry warhead." @default.
- W2762795063 created "2017-10-20" @default.
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- W2762795063 date "2017-01-01" @default.
- W2762795063 modified "2023-09-23" @default.
- W2762795063 title "Optimizing design of configuration parameters for re-entry warhead considering multiple constraints" @default.
- W2762795063 doi "https://doi.org/10.1063/1.5005253" @default.
- W2762795063 hasPublicationYear "2017" @default.
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