Analysis of calculation results of lift and drag forces for several wings using nonlinear section data

    Egidijus Pakalnis Info
    Eduardas Lasauskas Info
    Jonas Stankūnas Info
DOI: https://doi.org/10.3846/16487788.2005.9635893

Abstract

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 aerodynamics

How to Cite

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

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March 31, 2005
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Copyright (c) 2005 The Author(s). Published by Vilnius Gediminas Technical University.

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Published

2005-03-31

Issue

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

Section

Articles

Copyright

Copyright (c) 2005 The Author(s). Published by Vilnius Gediminas Technical University.

License

Creative Commons License
This work is licensed under a Creative Commons Attribution 4.0 International License.

How to Cite

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

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