| Citation: | YUAN Y，LIU J，YU J Q，et al. Aerodynamic layout optimization design of high-speed folding-wing vehicles[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（11）：3410-3416 （in Chinese） doi: 10.13700/j.bh.1001-5965.2022.0849
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In order to solve the optimization design problem of the aerodynamic layout of complex high-speed folding-wing vehicles under the constraints of internal loads and external launch devices, a parametric modeling method for folding-wing vehicles based on the combination of class shape transformation (CST) and direct parameterization was proposed. In addition, a fast calculation method of viscous aerodynamic characteristics based on the rapid correction of the normal vector of the object plane was developed. The multi-objective optimization algorithm framework and optimization process of high-speed folding-wing vehicles based on Kriging-genetic algorithm (Kriging-GA) were constructed, so as to optimize the aerodynamic layout design of high-speed folding-wing vehicles. The optimization solution set under multiple objectives and constraints was obtained, which could guide the aerodynamic layout optimization design of high-speed folding-wing vehicles.
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