Flight Dynamic Coupling

Flight Dynamic Coupling is a rotor aeroelastic phenomenon in which the dynamic response of the rotor blades interacts with the rigid-body flight dynamics of the aircraft, leading to mutually influencing oscillatory modes that can alter stability, control, and handling characteristics.

16

Publications

518

Citations

46

Authors

23

Institutions

Publications per year

2017–2026

3

Authors

46

  1. MC
    Mark Costello

    Georgia Institute of Technology, United States

    3 publications · 118 citations

    3

    h-index

  2. NT
    Nhan T. Nguyen

    Ames Research Center, United States

    2 publications · 29 citations

    2

    h-index

  3. LB
    Lewis B. Schiff

    Ames Research Center, United States

    2 publications · 42 citations

    2

    h-index

  4. JS
    Jubaraj Sahu

    DEVCOM Army Research Laboratory, United States

    2 publications · 44 citations

    2

    h-index

  5. NM
    Neal M. Chaderjian

    Ames Research Center, United States

    2 publications · 42 citations

    2

    h-index

1–5 of 46

Venues

  1. Journal of Aircraft

    4 publications · 113 citations

    4

    h-index

  2. AIAA Atmospheric Flight Mechanics Conference and Exhibit

    Conference · 2 publications · 41 citations

    2

    h-index

  3. Sensors

    1 publications · 17 citations

    1

    h-index

  4. 33rd AIAA Applied Aerodynamics Conference

    Conference · 1 publications · 13 citations

    1

    h-index

  5. IEEE Transactions on Industrial Electronics

    1 publications · 114 citations

    1

    h-index

1–5