Tail Structural Loads

Tail Structural Loads is a structural engineering construct that quantifies the distributed forces and moments acting on the tail section of an aerospace vehicle during flight, distinguishing it from other airframe load analyses by focusing specifically on aerodynamic, inertial, and control surface-induced stresses inherent to tail assemblies.

7

Publications

179

Citations

25

Authors

6

Institutions

Publications per year

2017–2026

0

Authors

25

  1. EV
    E. V. Laitone

    University of California, Berkeley, United States

    1 publications · 21 citations

    1

    h-index

  2. KP
    K. Pinori

    ITER, France

    1 publications · 18 citations

    1

    h-index

  3. DW
    Donald W. Rhoads

    Cornell University, United States

    1 publications · 48 citations

    1

    h-index

  4. JS
    John Schuler

    University of Alaska Fairbanks, United States

    1 publications · 48 citations

    1

    h-index

  5. NP
    N. Pelletier

    Assystem (France), France

    1 publications · 18 citations

    1

    h-index

1–5 of 25

Venues

  1. Journal of the Franklin Institute

    1 publications · 21 citations

    1

    h-index

  2. Space Science Reviews

    1 publications · 34 citations

    1

    h-index

  3. Journal of Aircraft

    1 publications · 21 citations

    1

    h-index

  4. 1

    h-index

  5. Fusion Engineering and Design

    1 publications · 18 citations

    1

    h-index

1–5