Aircraft Trim

Aircraft Trim is a steady-state flight condition in which all forces and moments acting on an aircraft are balanced, resulting in equilibrium with no acceleration or rotational motion.

171

Publications

6.2K

Citations

387

Authors

112

Institutions

Publications per year

2017–2026

32

Authors

387

  1. DH
    Dewey H. Hodges

    Georgia Institute of Technology, United States

    10 publications · 1K citations

    10

    h-index

  2. NA
    N. Ananthkrishnan

    Indian Institute of Technology Bombay, India

    6 publications · 232 citations

    6

    h-index

  3. AD
    Atilla Dogan

    The University of Texas at Arlington, United States

    6 publications · 100 citations

    6

    h-index

  4. MP
    Mayuresh Patil

    Virginia Tech, United States

    5 publications · 828 citations

    5

    h-index

  5. CE
    Carlos E. S. Cesnik

    University of Michigan, United States

    5 publications · 498 citations

    5

    h-index

1–5 of 387

Venues

  1. Journal of Aircraft

    35 publications · 1.8K citations

    21

    h-index

  2. Journal of Guidance Control and Dynamics

    8 publications · 706 citations

    8

    h-index

  3. Aerospace Science and Technology

    AST · 5 publications · 158 citations

    5

    h-index

  4. AIAA Journal

    5 publications · 201 citations

    5

    h-index

  5. NASA Technical Reports Server (NASA)

    Repository · 6 publications · 81 citations

    5

    h-index

1–5