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- W2326469355 abstract "The present study evaluates the consideration of propeller slipstream effects in a structural optimization procedure as commonly used in integrated preliminary aircraft design. Therefore an optimization model comprising aerodynamic and structural analysis of an exemplary short range aircraft wing box is developed. The aerodynamic loads are calculated with a potential-based 3D-panel code employing an actuator disk vortex tube and membrane arrangement for reflection of the propeller slipstream influence. Structural analysis is provided by means of a finite element model. The comparison of stress distributions and wing box masses obtained with and without incorporation of the propeller slipstream model indicate a distinct influence of the latter on the optimization result and thus on the entire underlying preliminary aircraft design process." @default.
- W2326469355 created "2016-06-24" @default.
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- W2326469355 date "2013-06-22" @default.
- W2326469355 modified "2023-09-25" @default.
- W2326469355 title "Influence of Propeller Aerodynamics on Structural Wing Box Optimization in Integrated Preliminary Aircraft Design" @default.
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- W2326469355 doi "https://doi.org/10.2514/6.2013-2521" @default.
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