Convergence of lift force calculation of a tapered wing using non-linear section data

Authors

  • E. Pakalnis Vilnius Gediminas Technical University
  • E. Lasauskas Vilnius Gediminas Technical University
  • J. Stankūnas Vilnius Gediminas Technical University

Abstract

The article presents some peculiarities of lift force calculation method using nonlinear section data. The main task is to determine an influence of iteration procedure on solution accuracy. This evaluation is a part of initiated research on potentials and application limits of the method. Set of accuracy is described in more details. Influence results of iteration procedure are presented for lift calculation of a tapered wing.

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Published

2005-02-17

Issue

Vol. 51 No. 1 (2005)

Section

Articles

License

The copyright for the articles in this journal is retained by the author(s) with the first publication right granted to the journal. The journal is licensed under the Creative Commons Attribution License 4.0 (CC BY 4.0).