Flap-deflection Trim

Flap-Deflection Trim is a flight control trim strategy within aircraft longitudinal stability and control analysis that specifically adjusts the deflection angle of trailing-edge flaps to balance aerodynamic moments and achieve equilibrium in pitch attitude without continuous elevator input.

3

Publications

56

Citations

6

Authors

2

Institutions

Publications per year

2017–2026

1

Authors

6

  1. FG
    Farhan Gandhi

    Pennsylvania State University, United States

    1 publications · 11 citations

    1

    h-index

  2. MP
    Marvin P. Jentzsch

    University of Arizona, United States

    1 publications · 31 citations

    1

    h-index

  3. JE
    James E. Bluman

    University of Alabama in Huntsville, United States

    1 publications · 11 citations

    1

    h-index

  4. IW
    I. Wygnanski

    University of Arizona, United States

    1 publications · 31 citations

    1

    h-index

  5. RC
    Roberto Celi

    University of Maryland, College Park, United States

    1 publications · 14 citations

    1

    h-index

1–5 of 6

Institutions

2

  1. University of Maryland, College Park

    College Park, United States

    1 h-index

    1 publications

    14 citations

  2. University of Arizona

    Tucson, United States

    1 h-index

    3 publications

    93 citations

  3. Warsaw University of Technology

    Warsaw, Poland

    1 publications

    12 citations

1–3 of 2

Venues

  1. Journal of Guidance Control and Dynamics

    1 publications · 14 citations

    1

    h-index

  2. AIAA Journal

    1 publications · 31 citations

    1

    h-index

  3. Journal of the American Helicopter Society

    1 publications · 11 citations

    1

    h-index

  4. Aircraft Engineering and Aerospace Technology

    1 publications · 12 citations

1–4