Trim Analysis

Trim Analysis is a systematic computational or analytical method employed within aircraft performance and stability studies to determine the equilibrium flight conditions under which all aerodynamic, inertial, and propulsion forces and moments balance, enabling steady or prescribed maneuvering flight.

54

Publications

2.4K

Citations

138

Authors

63

Institutions

Publications per year

2017–2026

15

Authors

138

  1. NA
    N. Ananthkrishnan

    Indian Institute of Technology Bombay, India

    4 publications · 96 citations

    4

    h-index

  2. DN
    Dimitri N. Mavris

    Georgia Institute of Technology, United States

    3 publications · 83 citations

    3

    h-index

  3. AB
    Afshin Banazadeh

    Sharif University of Technology, Iran

    2 publications · 25 citations

    2

    h-index

  4. WH
    Wen-Jing Hsu

    Nanyang Technological University, Singapore

    2 publications · 29 citations

    2

    h-index

  5. CE
    Charles E. Leiserson

    Massachusetts Institute of Technology, United States

    2 publications · 82 citations

    2

    h-index

1–5 of 138

Venues

  1. Journal of Aircraft

    9 publications · 317 citations

    9

    h-index

  2. AIAA Atmospheric Flight Mechanics Conference and Exhibit

    Conference · 2 publications · 31 citations

    2

    h-index

  3. Journal of Guidance Control and Dynamics

    2 publications · 203 citations

    2

    h-index

  4. AIAA SCITECH 2022 Forum

    Conference · 2 publications · 27 citations

    2

    h-index

  5. International Journal of Micro Air Vehicles

    2 publications · 72 citations

    2

    h-index

1–5