Airfoil Analysis and Effect of Wing Shape Optimization on Aerodynamic Parameters in a Steady Flight

Airfoil Analysis and Effect of Wing Shape Optimization on Aerodynamic Parameters in a Steady Flight

Vishu K. Oza

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Hardik R. Vala

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α Silver Oak University, Gujarat, India.

Airfoil Analysis and Effect of Wing Shape Optimization on Aerodynamic Parameters in a Steady Flight

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Abstract

The work in this paper deals with reconstructing and optimizing the wing geometry of an Unmanned Combat Aerial Vehicle for improved performance and reviewing the impact of the modification on flight parameters in a steady flight. The behavior of airfoils at planned flight conditions under I.S.A. is checked in XFLR5 software. Following up by 2-D CFD and boundary layer analysis of former and new airfoil, dimensions of the wing are re-developed, keeping the fuselage and tail structure same. The existing wing and the optimized wing design is analyzed by Vortex Lattice Method and Triangular Panel Method, with an objective to make the shape of the wing aerodynamically suitable for an increased Lift to Drag ratio and thereby minimizing drag coefficients.

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Funding

No external funding was declared for this work.

Conflict of Interest

The authors declare no conflict of interest.

Ethical Approval

No ethics committee approval was required for this article type.

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Not applicable for this article.

How to Cite This Article

Vishu K. Oza. 2021. \u201cAirfoil Analysis and Effect of Wing Shape Optimization on Aerodynamic Parameters in a Steady Flight\u201d. Global Journal of Research in Engineering - D: Aerospace Science GJRE-D Volume 21 (GJRE Volume 21 Issue D1): .

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GJRE Volume 21 Issue D1
Pg. 43- 53

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Crossref Journal DOI 10.17406/gjre

Print ISSN 0975-5861

e-ISSN 2249-4596

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GJRE-D Classification: FOR Code: 290201

Submission ReceivedDecember 10, 2020
Peer Review Double Blind
Handling Editor
Accepted January 1, 2021
Published January 15, 2021

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January 28, 2021

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