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

    Egidijus Pakalnis Affiliation
    ; Eduardas Lasauskas Affiliation
    ; Jonas Stankūnas Affiliation

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

Keyword : 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
Published in Issue
Mar 31, 2005
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This work is licensed under a Creative Commons Attribution 4.0 International License.