AERODYNAMIC ANALYSIS OF A SUBSONIC AIRCRAFT WING USING COMPUTATIONAL FLUID MODELLING
Küçük Resim Yok
Tarih
2024
Yazarlar
Dergi Başlığı
Dergi ISSN
Cilt Başlığı
Yayıncı
EUROSIS-ETI
Erişim Hakkı
info:eu-repo/semantics/closedAccess
Özet
Aircraft designers are mainly interested in finding the level of pressure, stresses and deformations of the parts of the aircraft, especially the wing, as in many aviation accidents, the failure of the wing was the main cause of disasters due to the aerodynamic loading. In this work, the numerical study was achieved to obtain the aerodynamic loading, span wise and chord wise. In this respect, the volume method was used to predict the pressure distribution of the wing in the subsonic potential flow. The singularity strength which satisfies the boundary condition of the tangential flow at the control point for a given Mach number and the angle of attack was employed in the package in which the design was achieved using the 3D geometry model by using the Software SOLIDWORKS 2020 and the second step was processing the governing differential equations for airflow over a wing by ANSYS FLUENT 2022 R1 version solver by utilizing a Finite Element Method. Finally, the results were compared with other research which have shown to be in good agreement. © 2024, EUROSIS-ETI. All rights reserved.
Açıklama
18th International Middle Eastern Simulation and Modelling Conference, MESM 2023 -- 20 November 2023 through 23 November 2023 -- Baghdad -- 315679
Anahtar Kelimeler
Aerodynamics, ANSYS, CFD, Mach Number
Kaynak
The International Middle Eastern Simulation and Modelling Conference, MESM 2023
WoS Q Değeri
Scopus Q Değeri
N/A
