Trim Conditions

Trim Conditions is a steady-state flight condition in which all aerodynamic forces and moments acting on an aircraft are balanced, resulting in zero net acceleration and zero angular acceleration, thereby enabling equilibrium flight.

105

Publications

3.6K

Citations

269

Authors

117

Institutions

Publications per year

2017–2026

22

Authors

269

  1. SF
    Sergey F. Golovashchenko

    Ford Motor Company (United States), United States

    4 publications · 96 citations

    4

    h-index

  2. HG
    Harry G. Kwatny

    Drexel University, United States

    3 publications · 41 citations

    3

    h-index

  3. GX
    Guohua Xu

    Nanjing University of Aeronautics and Astronautics, China

    3 publications · 82 citations

    3

    h-index

  4. AD
    Atilla Dogan

    The University of Texas at Arlington, United States

    3 publications · 47 citations

    3

    h-index

  5. NA
    N. Ananthkrishnan

    Indian Institute of Technology Bombay, India

    2 publications · 89 citations

    2

    h-index

1–5 of 269

Venues

  1. Journal of Aircraft

    11 publications · 264 citations

    10

    h-index

  2. Journal of Guidance Control and Dynamics

    5 publications · 424 citations

    5

    h-index

  3. Aerospace Science and Technology

    AST · 5 publications · 169 citations

    5

    h-index

  4. Journal of Materials Processing Technology

    5 publications · 142 citations

    5

    h-index

  5. Ocean Engineering

    4 publications · 128 citations

    4

    h-index

1–5