Tail Load Analysis

Tail Load Analysis is a methodological framework within aerospace engineering that systematically evaluates the aerodynamic and structural forces acting on an aircraft's tail section under various flight conditions to ensure stability and control.

15

Publications

901

Citations

38

Authors

17

Institutions

Publications per year

2017–2026

0

Authors

38

  1. RW
    Robert W. Moses

    Langley Research Center, United States

    2 publications · 29 citations

    2

    h-index

  2. MA
    Mark Anthony McComb

    Mississippi College, United States

    2 publications · 507 citations

    2

    h-index

  3. MB
    M. Bayon de Noyer

    Georgia Institute of Technology, United States

    1 publications · 16 citations

    1

    h-index

  4. AS
    Anja Struyf

    University of Antwerp, Belgium

    1 publications · 97 citations

    1

    h-index

  5. RF
    R. Feldman

    Mississippi College, United States

    1 publications · 99 citations

    1

    h-index

1–5 of 38

Venues

  1. Journal of Aircraft

    2 publications · 39 citations

    2

    h-index

  2. Technometrics

    2 publications · 507 citations

    2

    h-index

  3. 30th Structures, Structural Dynamics and Materials Conference

    Conference · 1 publications · 59 citations

    1

    h-index

  4. Progress in Aerospace Sciences

    1 publications · 42 citations

    1

    h-index

  5. Primates

    1 publications · 19 citations

    1

    h-index

1–5