Effect of wing deformation on aerodynamic loads at supersonic speeds

Date

2017-09-22

Author

Özkökdemir, Emir
Kurtuluş, Dilek Funda

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Aerodynamic performance of wings is directly related to the flow characteristics and the wing geometry. The change in the wing geometry by external loads such as the temperature gradient formed by aerodynamic heating and the pressure distribution on wing surfaces affect the flow characteristics around the wing. In addition, the change in the flow characteristics affects the structural and the thermal loading on the wing. Therefore, aerodynamic performance for undeformed wing has not the same performance as the deformed wing configuration. In the current study, a wing based on NACA65-009 airfoil is selected as a test case at zero angle of attack. Two and three dimensional flow characteristics are investigated. Effect of the three dimensional deformation on aerodynamic performance is presented.

URI

https://hdl.handle.net/11511/87777

Conference Name

Ankara International Aerospace Conference, (20 - 22 Eylül 2017)

Collections

Department of Aerospace Engineering, Conference / Seminar

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Citation Formats

E. Özkökdemir and D. F. Kurtuluş, “Effect of wing deformation on aerodynamic loads at supersonic speeds,” presented at the Ankara International Aerospace Conference, (20 - 22 Eylül 2017), Ankara, Türkiye, 2017, Accessed: 00, 2021. [Online]. Available: https://hdl.handle.net/11511/87777.