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- W2080695564 abstract "Abstract : This paper focuses on the demonstration of a new integrated aero-structural design method for aerospace vehicles. The approach combines an aero-structural analysis solver, a coupled aero-structural adjoint solver, a geometry-based analysis and design integration strategy, and an efficient gradient-based optimization algorithm. The aero-structural solver ensures highly accurate solutions by using high-fidelity models for both disciplines as well as a high-fidelity coupling procedure. The Euler equations are solved for the aerodynamics and a detailed finite element model is used for the primary structure. The coupled aero-structural adjoint solution is used to calculate the needed sensitivities of aerodynamic and structural cost functions with respect to both aerodynamic shape and" @default.
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- W2080695564 date "2002-06-26" @default.
- W2080695564 modified "2023-09-25" @default.
- W2080695564 title "Complete Configuration Aero-Structural Optimization Using a Coupled Sensitivity Analysis Method" @default.
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- W2080695564 doi "https://doi.org/10.2514/6.2002-5402" @default.
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