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• W4220823193 abstract "The truss-braced-wing (TBW) aircraft is a promising innovative design for the next-generation airliner. Nevertheless, for a full TBW wing–body–tail configuration, it is still a challenge to perform the comprehensive refined aerodynamic design. Especially, the complex mutual interference among the wing, struts, and fuselage should be analyzed in detail. Meanwhile, for its one-design cruise condition with and , the aerodynamic explorations and performances of drag divergence and near-buffet-onset condition are also fateful. To address these issues, we utilize high-fidelity Reynolds-averaged Navier–Stokes solver and gradient-based optimizer to conduct aerodynamic optimization designs, including a single-point optimization, a two-point optimization, and a three-point optimization. Results indicate that the single-point design obtains a nearly shock-free configuration with an approximate elliptical lift distribution and an of 24.09. Also, the refined local aerodynamic analyses lead to a good understanding of the complicated interactions with several junctions. For multipoint optimizations, both optimized configurations have the same level aerodynamic behavior on cruise condition compared with the single-point result, and they have a satisfying performance of drag divergence. Moreover, the three-point optimization design shows excellent aerodynamic efficiency with some extra off-design points evaluations, whereas the two-point optimization still has an undesirable off-design result." @default.
• W4220823193 created "2022-04-03" @default.
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• W4220823193 date "2022-09-01" @default.
• W4220823193 modified "2023-09-29" @default.
• W4220823193 title "Multipoint Aerodynamic Shape Optimization of a Truss-Braced-Wing Aircraft" @default.
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• W4220823193 doi "https://doi.org/10.2514/1.c036413" @default.
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