Tail Aeroelasticity

Tail Aeroelasticity is a specialized aeroelastic phenomenon characterized by the dynamic interaction between aerodynamic forces, structural elasticity, and inertial effects specific to the tail section of an aircraft, distinguishing it from aeroelastic behaviors in other airframe components.

6

Publications

250

Citations

21

Authors

11

Institutions

Publications per year

2017–2026

1

Authors

21

  1. DA
    Douglas A. Henderson

    United States Air Force Research Laboratory, United States

    2 publications · 72 citations

    2

    h-index

  2. RW
    Robert W. Moses

    Langley Research Center, United States

    1 publications · 36 citations

    1

    h-index

  3. DG
    D. G. Zimcik

    National Research Council Canada, Canada

    1 publications · 36 citations

    1

    h-index

  4. KS
    K. S. Nagaraja

    Wright-Patterson Air Force Base, United States

    1 publications · 36 citations

    1

    h-index

  5. SH
    S. Hanagud

    Georgia Institute of Technology, United States

    1 publications · 36 citations

    1

    h-index

1–5 of 21

Venues

  1. 1

    h-index

  2. AIAA Journal

    1 publications · 36 citations

    1

    h-index

  3. Animal Behaviour

    1 publications · 137 citations

    1

    h-index

  4. European Journal of Mechanics - B/Fluids

    1 publications · 20 citations

    1

    h-index

  5. Journal of the American Helicopter Society

    1 publications · 11 citations

    1

    h-index

1–5