Wing area optimization for box wing aircraft

  • Authors

    • Jemitola Paul Olugbeji Air Force Institute of Technology
    • Okafor Ekene Gabriel Air Force Institute of Technology
    • Godwin Abbe Air Force Institute of Technology
    2019-04-12
    https://doi.org/10.14419/ijet.v7i4.17147
  • Algorithm, Box wing, Optimization, Regression analysis, Wing area.

  • Abstract

    The optimization of the wing area of a medium range box wing aircraft was carried out in this study using a multidisciplinary conceptual design/optimization approach based on gradient search algorithm and regression analysis. The methodology was also applied to a similar sized conventional cantilever wing aircraft and the result generated an optimal wing area similar to the real wing area of the cantilever aircraft considered, thereby validating the methodology.

     

    Nomenclature

    AUM: All up Mass

    DOC: Direct Operating Cost

    CDo: Zero Lift Drag Coefficient

    : Wing Sweep Angle

    : Wing Average Thickness to Chord Ratio

    Subscript

    : Aft Wing

    F: Fore Wing

     


  • References

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  • How to Cite

    Paul Olugbeji, J., Ekene Gabriel, O., & Abbe, G. (2019). Wing area optimization for box wing aircraft. International Journal of Engineering & Technology, 7(4), 5679-5682. https://doi.org/10.14419/ijet.v7i4.17147

    Received date: 2018-08-08

    Accepted date: 2019-03-30

    Published date: 2019-04-12