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- W2382715436 abstract "The aerodynamics design methods of wing for large transport aircraft are researched and developed in this paper.An improved inverse design method based on Takanashi's iterative residual correction principle is developed to design supercritical wing for large transport aircraft,meanwhile a optimization method is developed to design low speed high-lift configuration of wing,which combines the optimization method with the distributed parallel computing in LAN(local-area-network) to enhance the efficiency.Design examples show that the design method is feasible and provide practical tool for the aerodynamics design of wing for large transport aircraft." @default.
- W2382715436 created "2016-06-24" @default.
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- W2382715436 date "2009-01-01" @default.
- W2382715436 modified "2023-09-23" @default.
- W2382715436 title "Aerodynamic Design of Wing for Large Transport Aircraft" @default.
- W2382715436 hasPublicationYear "2009" @default.
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