Aerodynamic Performance of a Tail-less Blended Wing-Body Small Transport Aircraft

Authors

  • Atikah Basyirah Abdul Muta’ali Aviation Technology Research Group, Flight Technology and Test Centre (FTTC), Faculty of Mechanical Engineering, Universiti Teknologi MARA (UiTM), 40450 Shah Alam, Selangor, Malaysia
  • Rizal Effendy Mohd Nasir Aviation Technology Research Group, Flight Technology and Test Centre (FTTC), Faculty of Mechanical Engineering, Universiti Teknologi MARA (UiTM), 40450 Shah Alam, Selangor, Malaysia
  • Wirachman Wisnoe Aviation Technology Research Group, Flight Technology and Test Centre (FTTC), Faculty of Mechanical Engineering, Universiti Teknologi MARA (UiTM), 40450 Shah Alam, Selangor, Malaysia
  • Wahyu Kuntjoro Aviation Technology Research Group, Flight Technology and Test Centre (FTTC), Faculty of Mechanical Engineering, Universiti Teknologi MARA (UiTM), 40450 Shah Alam, Selangor, Malaysia

Keywords:

blended-wing body, lift to drag ratio, transport aircraft

Abstract

Blended wing-body (BWB) is a concept with promising future for transport aircraft. Many studies have been conducted on blended wing body concept, each with different ideas and designs. The search of the perfect BWB design is still on going around the world with the hope of applying the design to the conventional aviation industries. This paper proposes a tail-less BWB-type aircraft design to be used as transport aircraft with similar payload capacity as the popular conventional DHC-6 Twin Otter aircraft. An experimental investigation is conducted to obtain aerodynamic characteristics and performance of the proposed BWB aircraft design, known as Baseline-IX, and its conventional counterpart. Both aircrafts have the same wing span and cargo-passenger volume in the fuselage. The models are both 1:30 scale with experiment conducted at 36 m/s in LST-1 wind tunnel at Flight Technology & Test Centre laboratory. Discussions on aerodynamic characteristics comparison between Baseline-IX BWB and DHC-6 concluded that although the former is only 8.25% better in term of lift-to-drag ratio than the latter, the CL 3/CD 2 of Baseline-IX is 31.7% higher than DHC6’s. This means that for a given take-off weight, the Baseline-IX will have 8.25% better range and 31.7% better endurance than its conventional counterpart. At maximum endurance, the Baseline-IX also flies slower indicating that it may also be used surveillance or maritime patrol aircraft that requires long hours of flight.

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Published

2020-12-25

How to Cite

Abdul Muta’ali, A. B. ., Mohd Nasir, R. E. ., Wisnoe, W. ., & Kuntjoro, W. . (2020). Aerodynamic Performance of a Tail-less Blended Wing-Body Small Transport Aircraft. Journal of Advanced Research in Fluid Mechanics and Thermal Sciences, 66(1), 135–150. Retrieved from https://www.akademiabaru.com/submit/index.php/arfmts/article/view/2814

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Articles