Structural Analysis of a Transport Aircraft Wing | ||||
| The International Undergraduate Research Conference | ||||
| Article 2, Volume 2, Second International Undergraduate Research Conference, IUGRC, 2017, Page 31-31 PDF (466.96 K) | ||||
| Document Type: Original Article | ||||
| DOI: 10.21608/iugrc.2017.90572 | ||||
 View on SCiNiTO | ||||
| Authors | ||||
| Alnazir Khalafallah Alatta1; Mohammed Alnazir Abd Algader1; Tariq Hassan Alsonni2; Abdul Aziz Abdul Majid Sulieman3 | ||||
| 1Aeronautical Engineering Department, Engineering College, Karary University, Khartoum, Sudan. | ||||
| 2PHD, International College of Science and Technology, Khartoum, Sudan. | ||||
| 3Aeronautical Engineering Department, Engineering College, Karary University, Khartoum, Sudan | ||||
| Abstract | ||||
| In this study the procedures of structural analysis of a typical transport aircraft wing has been followed. Firstly, the wing model has been drawn using CATIA® V5, this model consists of several structural components such as spars, ribs and skin. Secondly, the model has been exported into structural analysis software ANSYS ® 2016. Thirdly, pressure distribution has been created using MATLAB code (panel method) & CFD file data (fluent).and applied on the model. Finally The stresses, strains, deformations and safety factors where obtained for the model, it is found that the obtained stresses caused by the aerodynamic loads on the wing are within the design structural limits where the failure by yield or buckling has not been occurred. Keywords- structural, wing, pressure distribution. | ||||
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