Calculation results for 11 different finite span wings are presented. Calculations were made by a combination of a numerical solution of lifting line theory with a technique developed to evaluate nonlinear section lift data. Aerodynamic coefficients for these wings are compared to the research results of other authors and to experimental data. First Published Online: 14 Oct 2010
Analysis of calculation results of lift and drag forces for several wings using nonlinear section data
2005
Article (Journal)
Electronic Resource
Unknown
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