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Analysis of calculation results of lift and drag forces for several wings using nonlinear section data
Vol 9 No 1 (2005): Proceedings of the sixth international seminar on “Recent Research and Design Progress in Aeronautical Engineering and its Influence on Education“ – Riga, Latvia
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.
Pakalnis, E., Lasauskas, E., & Stankūnas, J. (2005). Analysis of calculation results of lift and drag forces for several wings using nonlinear section data. Aviation, 9(1), 26-31. https://doi.org/10.3846/16487788.2005.9635893
This is an Open Access article distributed under the terms of the Creative Commons Attribution License (http://creativecommons.org/licenses/by/4.0/), which permits unrestricted use, distribution, and reproduction in any medium, provided the original author and source are credited.
