| OPTIMAL DESIGN AND AERODYNAMIC CALCULATION OF WING CONFIGURATION OF CIVIL AIRCRAFT |
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| 引用本文： | Wang Liangyi(Department of Aerddynamics,NUAA 29 Yudao Street,Nanjing 210016,P.R.China). OPTIMAL DESIGN AND AERODYNAMIC CALCULATION OF WING CONFIGURATION OF CIVIL AIRCRAFT[J]. 南京航空航天大学学报(英文版), 1994, 0(2) |
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| 作者姓名： | Wang Liangyi(Department of Aerddynamics NUAA 29 Yudao Street Nanjing 210016 P.R.China) |
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| 作者单位： | Department of Aerddynamics，NUAA 29 Yudao Street，Nanjing 210016，P.R.China |
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| 摘 要： | ＯＰＴＩＭＡＬＤＥＳＩＧＮＡＮＤＡＥＲＯＤＹＮＡＭＩＣＣＡＬＣＵＬＡＴＩＯＮＯＦＷＩＮＧＣＯＮＦＩＧＵＲＡＴＩＯＮＯＦＣＩＶＩＬＡＩＲＣＲＡＦＴ￥ＷａｎｇＬｉａｎｇｙｉ（ＤｅｐａｒｔｍｅｎｔｏｆＡｅｒｄｄｙｎａｍｉｃｓ，ＮＵＡＡ２９ＹｕｄａｏＳｔｒｅ...
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OPTIMAL DESIGN AND AERODYNAMIC CALCULATION OF WING CONFIGURATION OF CIVIL AIRCRAFT |
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| Wang Liangyi. OPTIMAL DESIGN AND AERODYNAMIC CALCULATION OF WING CONFIGURATION OF CIVIL AIRCRAFT[J]. Transactions of Nanjing University of Aeronautics & Astronautics, 1994, 0(2) |
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| Authors: | Wang Liangyi |
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| Abstract: | An effective method of optimal design of wing configuration is provided. The SUMT (sequential unconstained minimization technique) method is a good technique for solving the nonlinear programming. The application of penalty in optimal design of wing configuration has been solved well. The present method for the aerodynamic calculation is the combination of both the nonlinear panel method and the suction analogy method of vortexlift spanwise distribution on large swept wing-tip. The calculation results are in good agreement with experimental data. According to the computation and experiment,the mechanism of the increased lift and reduced drag about the sheared wing-tip wing has been analyzed, and some opinions of interest are proposed. |
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| Keywords: | optimum design aerodynamic computations civil aircraft sheared wing-tip wing penalty function |
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