Analysis of calculation results of lift and drag forces for several wings using nonlinear section data
DOI: https://doi.org/10.3846/16487788.2005.9635893Abstract
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
Keywords:
lift, drag, wing, non-linear aerodynamicsHow to Cite
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Copyright (c) 2005 The Author(s). Published by Vilnius Gediminas Technical University.
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Copyright (c) 2005 The Author(s). Published by Vilnius Gediminas Technical University.
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This work is licensed under a Creative Commons Attribution 4.0 International License.