Analytical method in the linear three-dimentional aerodynamics of a thin wing with winglets

Authors

UDC

533.69

EDN

UDUZEL

DOI:

10.31429/vestnik-21-1-41-46

Abstract

The paper presents an analytical method in the classical problem of flow around a thin rectangular plate with and without winglets. There is described the method for calculating inductive reactance of the thin plate. The method for calculating the suction force, to calculate the inductive reactance of the plate with winglets is considered. There is also described a discretization of equations, to calculate inductive reactance. Then we demonstrate a comparison of the aerodynamic quality for plates with and without winglets. After that, we give some conclusions about the influence of winglets on the aerodynamic quality of the thin plate with winglets, taking into account the suction force.

Keywords:

aerodynamics, thin rectangular plate, winglets, lifting force, aerodynamic quality

Funding information

The study did not have any sponsorship.

Authors info

  • Ilya Samsonov

    postgraduate student of Department of Theoretical and Computational Hydroaerodynamics, Vorovich Institute of Mathematics, Mechanics and Computer Science, Southern Federal University

  • Mezhlum Sumbatyan

    Ph.D (Physical and Mathematical), Professor of a Department of Theoretical and Computational Hydroaerodynamics, Vorovich Institute of Mathematics, Mechanics and Computer Science, Southern Federal University

References

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Issue

Pages

41-46

Section

Mechanics

Dates

Submitted

March 12, 2024

Accepted

March 18, 2024

Published

March 27, 2024

How to Cite

[1]
Samsonov, I., Sumbatyan, M., Analytical method in the linear three-dimentional aerodynamics of a thin wing with winglets. Ecological Bulletin of Research Centers of the Black Sea Economic Cooperation, 2024, т. 21, № 1, pp. 41–46. DOI: 10.31429/vestnik-21-1-41-46

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