Rotor Trim Analysis

Rotor Trim Analysis is a computational methodology in rotorcraft aerodynamics that determines the steady-state flight conditions and control inputs required to achieve equilibrium in forces and moments by iteratively adjusting rotor collective and cyclic pitch angles, fuselage orientation, and flight velocity while satisfying aerodynamic, inertial, and propulsive balance constraints.

39

Publications

1.2K

Citations

98

Authors

30

Institutions

Publications per year

2017–2026

9

Authors

98

  1. FG
    Farhan Gandhi

    Pennsylvania State University, United States

    3 publications · 68 citations

    3

    h-index

  2. IC
    Inderjit Chopra

    University of Maryland, College Park, United States

    3 publications · 91 citations

    3

    h-index

  3. JW
    Joon W. Lim

    Ames Research Center, United States

    2 publications · 44 citations

    2

    h-index

  4. GX
    Guohua Xu

    Nanjing University of Aeronautics and Astronautics, China

    2 publications · 25 citations

    2

    h-index

  5. YS
    Yongjie Shi

    Nanjing University of Aeronautics and Astronautics, China

    2 publications · 25 citations

    2

    h-index

1–5 of 98

Venues

  1. Journal of Aircraft

    6 publications · 133 citations

    6

    h-index

  2. Journal of the American Helicopter Society

    5 publications · 242 citations

    5

    h-index

  3. AIAA Journal

    4 publications · 85 citations

    4

    h-index

  4. Journal of Guidance Control and Dynamics

    2 publications · 32 citations

    2

    h-index

  5. Aerospace Science and Technology

    AST · 2 publications · 46 citations

    2

    h-index

1–5