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- W2373095810 abstract "Forward-Swept wing(FSW) configuration provides a new direction for the aerodynamic configuration design of UAV because its excellent aerodynamic characteristics.The Class-Shape function Transformation(CST) method is used to describe the parameterized airfoil geometry.The parameterized models for aerodynamic and stealthy performance of FSW are constructed.The aerodynamic analysis model of FSW is constructed by computational fluid dynamics method based on N-S equations.The stealthy performance analysis model of FSW is constructed by computational electromagnetics method based Method of Moments(MoM).The multi-objective aerodynamic and stealthy performance optimization method for FSW using Kriging model is presented.The Latin hypercube method is employed to get a set of sample points.The aerodynamic and stealthy performance Kriging models are built.The multi-objective aerodynamic and stealthy performance optimization of FSW is optimized by combining Pareto genetic algorithm with Kriging model.The results of the investigation show that the constructed analysis models are reasonable and the presented multi-objective optimization design method is feasible,which can improve the performance of large-aspect-ratio FSW and the efficiency of optimization effectively." @default.
- W2373095810 created "2016-06-24" @default.
- W2373095810 creator A5061671556 @default.
- W2373095810 date "2011-01-01" @default.
- W2373095810 modified "2023-09-23" @default.
- W2373095810 title "Multi-objective Aerodynamic and Stealthy Performance Optimization for Large-aspect-ratio Forward-swept Wings" @default.
- W2373095810 hasPublicationYear "2011" @default.
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