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- W2320176684 abstract "The aircraft conceptual design process traditionally determines the size, shape, specification and configuration of an airframe to meet specific performance requirements. A successful design process must incorporate synthetic (generative) as well as analytic elements. In the conceptual design process the overall planform and span-wise thickness distribution of a wing must be defined. However, if the performance of the concept wing is to be properly verified, the wing geometry must exhibit approximately correct drag divergence behavior at an expected induced drag level. This paper describes a method to produce an approximate loft worthy of analysis using higher order methods, and draws some observations concerning the wing planform selection process." @default.
- W2320176684 created "2016-06-24" @default.
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- W2320176684 date "2010-06-26" @default.
- W2320176684 modified "2023-10-16" @default.
- W2320176684 title "A Rapid Synthesis Method to Develop Conceptual Design Transonic Wing Lofts" @default.
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- W2320176684 doi "https://doi.org/10.2514/6.2010-9025" @default.
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