The Application of Ansys-Fluent Software for Aerodynamic Analysis on Rectangular and Moderate Swept Wing Planform

Authors

  • M. Z. Md Shah Tun Hussein Onn University of Malaysia
  • B. Basuno Tun Hussein Onn University of Malaysia
  • A. Abdullah Tun Hussein Onn University of Malaysia
  • M. F. Pairan Tun Hussein Onn University of Malaysia

Abstract


ANSYS-Fluent software represents a CFD software having the capability for solving various engineering flow problems. Besides offering a variety of flow solvers, this software also offers various type of turbulence model can be used in the flow analysis. The present work focuses on the use of this software applied to two type wing models, a moderately swept wing and (2) a rectangular wing planform. The moderately swept wing geometry and experimental data were obtained from AGARD AR-138, whereas the rectangular wing planform was obtained from RTO-TR-026. The first model evaluated by using five different turbulent models, namely (1) Spalart-Allmaras, (2) k-ε Standard, (3) k-ε Realizable, (4) k-ω Standard and (5) k-ω SST turbulence models. Comparisons result with AGARD shows that all turbulent models are able to provide in a good agreement. However, Spalart-Allmaras and k-ω SST turbulence models give less CPU time than the others. These two turbulent models then applied to the case of a rectangular wing plan form. The result from the second test case, the k-ω SST turbulence models, give a more accurate result compared to the Spalart-Allmaras turbulence models. It gives a better result compared with the Spalart-Allmaras turbulence models. The k-ω SST turbulence model makes the ANSYS-Fluent result just differ 11.5% from the experiment result while for the Spalart-Allmaras turbulence model differs 14.05%.  Here it can be concluded that k-ω SST turbulence mode may represent a suitable turbulence model for solving flow over a rectangular wing to the moderate swept wing plan form.

Author Biography

M. Z. Md Shah, Tun Hussein Onn University of Malaysia

Mohd Zarif Md Shah currently is a doctoral student at the Tun Hussein Onn University of Malaysia, Faculty of Mechanical and Manufacturing Engineering. He received a bachelor’s degree from University Malaysia Perlis and a master’s degree from Tun Hussein Onn University of Malaysia, both in Mechanical Engineer. His current field is in aeronautic and aerodynamic studies specifically in computational fluid dynamics (CFD). Along with his doctoral studies, he become a part time warden for a pilot student in Asia Aeronatical Training Academy. When he’s not keeping busy with his studies and working, he love to make some studies in investment and financing

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Published

2021-07-09

How to Cite

Md Shah, M. Z., Basuno, B., Abdullah, A., & Pairan, M. F. (2021). The Application of Ansys-Fluent Software for Aerodynamic Analysis on Rectangular and Moderate Swept Wing Planform. Journal of Engineering and Technology (JET), 12(1), 11–32. Retrieved from https://jet.utem.edu.my/jet/article/view/6012