STRUCTURAL DEFORMATION ANALYSIS ON MORPHING MAV WING

Authors

  • Noor Iswadi Ismail Mechanical Engineering Studies, College of Engineering, Universiti Teknologi MARA, Cawangan Pulau Pinang, Kampus Permatang Pauh, Penang, Malaysia
  • M. Hisyam Basri Mechanical Engineering Studies, College of Engineering, Universiti Teknologi MARA, Cawangan Pulau Pinang, Kampus Permatang Pauh, Penang, Malaysia
  • Mahadzir M.M Mechanical Engineering Studies, College of Engineering, Universiti Teknologi MARA, Cawangan Pulau Pinang, Kampus Permatang Pauh, Penang, Malaysia.
  • Hazim Sharudin Mechanical Engineering Studies, College of Engineering, Universiti Teknologi MARA, Cawangan Pulau Pinang, Kampus Permatang Pauh, Penang, Malaysia.
  • Sharzali Che Mat Mechanical Engineering Studies, College of Engineering, Universiti Teknologi MARA, Cawangan Pulau Pinang, Kampus Permatang Pauh, Penang, Malaysia
  • Muhammad Arif Ab Hamid Pahmi Mechanical Engineering Studies, College of Engineering, Universiti Teknologi MARA, Cawangan Pulau Pinang, Kampus Permatang Pauh, Penang, Malaysia
  • Azmi Husin Mechanical Engineering Studies, College of Engineering, Universiti Teknologi MARA, Cawangan Pulau Pinang, Kampus Permatang Pauh, Penang, Malaysia
  • Rozaini Othman Mechanical Engineering Studies, College of Engineering, Universiti Teknologi MARA, Cawangan Pulau Pinang, Kampus Permatang Pauh, Penang, Malaysia

DOI:

https://doi.org/10.11113/jm.v46.488

Keywords:

Micro air vehicle, Twist morphing wing

Abstract

Micro air vehicles (MAV) and the notion of morphing are always changing to suit their mission characteristics. To achieve twist morphing, however, the process underlying the application of the morphing force and its related aerodynamic load is not well understood. In this study, the structural deformation of the washout twist morphing wing MAV was investigated, and the association between wing deformation, morphing force, and membrane inflation owing to aerodynamic force was clarified. Several numerical simulations of washout TM wings were undertaken and compared to those of rigid and membrane wings. The results demonstrated that twist morphing is associated with considerable wing deformation. In comparison to the TM 3N, TM 1N, and baseline wing, the TM 5N wing was the most distorted. The deformation of the wing structure was substantially influenced by the morphing force applied to the wing. Larger morphing power led to a greater degree of wing distortion.

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Published

2023-11-23

How to Cite

Ismail, N. I., M. Hisyam Basri, Mahadzir M.M, Sharudin, H., Che Mat, S., Ab Hamid Pahmi, M. A., … Othman, R. (2023). STRUCTURAL DEFORMATION ANALYSIS ON MORPHING MAV WING. Jurnal Mekanikal, 46(2), 62–71. https://doi.org/10.11113/jm.v46.488

Issue

Section

Mechanical