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- W2102685237 abstract "The automatic technique of a computational aeroelastics modeling was devised and applied to aero-structur al coupling problem of high aspect-ratio swept-back wing. The model of external and internal substructures with medium complexity are defined in parametric forms of design variables, and utilized for generating flowfield grids and structural finite elements. Flowfield and structure are connected by the mechanisms of exchanging each solution. The key techniques of surface tracking, flowfield deformation, solution interpolation, and structural generation have been described in this article. Also the application to transonic aircraft wing has been demonstrated. In this attempt, the simultaneous execution of fluid and structural programs was applied and about 60%-increase in execution speed compared with the serial execution was obtained. Nomenclature" @default.
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- W2102685237 date "1998-08-22" @default.
- W2102685237 modified "2023-10-16" @default.
- W2102685237 title "Coupled aero-structural model - Approach and application to high aspect-ratio wing-box structures" @default.
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- W2102685237 doi "https://doi.org/10.2514/6.1998-4837" @default.
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