Wing Twist Effects

Wing Twist Effects is a static aeroelastic phenomenon characterized by the alteration of an aircraft wing's aerodynamic performance due to elastic torsional deformation induced by aerodynamic loads, distinguishing it from other aeroelastic effects by its primary influence on lift distribution and stall characteristics through changes in local angle of attack.

33

Publications

1.1K

Citations

79

Authors

34

Institutions

Publications per year

2017–2026

6

Authors

79

  1. WF
    W. F. Phillips

    Utah State University, United States

    3 publications · 205 citations

    3

    h-index

  2. HC
    Hoon Cheol Park

    Konkuk University, South Korea

    3 publications · 151 citations

    3

    h-index

  3. TQ
    Tri Quang Truong

    Konkuk University, South Korea

    2 publications · 119 citations

    2

    h-index

  4. MS
    M. Spottiswoode

    Cranfield University, United Kingdom

    2 publications · 41 citations

    2

    h-index

  5. MC
    M.V. Cook

    Cranfield University, United Kingdom

    2 publications · 41 citations

    2

    h-index

1–5 of 79

Venues

  1. Journal of Aircraft

    7 publications · 270 citations

    7

    h-index

  2. Aerospace Science and Technology

    AST · 2 publications · 63 citations

    2

    h-index

  3. Journal of Experimental Biology

    2 publications · 210 citations

    2

    h-index

  4. Bioinspiration & Biomimetics

    2 publications · 65 citations

    2

    h-index

  5. NASA Technical Reports Server (NASA)

    Repository · 2 publications · 26 citations

    2

    h-index

1–5