Blade Flapping Dynamics

Blade Flapping Dynamics is a rotorcraft flight mechanics phenomenon characterized by the vertical out-of-plane motion of rotor blades about a flapping hinge or equivalent structural compliance, enabling the blade to respond to aerodynamic and inertial forces arising from asymmetric inflow, cyclic pitch, and forward flight conditions.

113

Publications

3.9K

Citations

227

Authors

90

Institutions

Publications per year

2017–2026

14

Authors

227

  1. KH
    Kurt Hohenemser

    Washington University in St. Louis, United States

    6 publications · 115 citations

    6

    h-index

  2. IC
    Inderjit Chopra

    University of Maryland, College Park, United States

    6 publications · 211 citations

    6

    h-index

  3. GH
    G. H. Gaonkar

    Washington University in St. Louis, United States

    5 publications · 113 citations

    5

    h-index

  4. PP
    Peretz P. Friedmann

    University of Michigan, United States

    4 publications · 76 citations

    4

    h-index

  5. NK
    Nikhil Koratkar

    Rensselaer Polytechnic Institute, United States

    3 publications · 98 citations

    3

    h-index

1–5 of 227

Venues

  1. Journal of the American Helicopter Society

    14 publications · 501 citations

    13

    h-index

  2. Journal of Aircraft

    5 publications · 81 citations

    5

    h-index

  3. AIAA Journal

    5 publications · 131 citations

    5

    h-index

  4. NASA Technical Reports Server (NASA)

    Repository · 5 publications · 108 citations

    5

    h-index

  5. Journal of Sound and Vibration

    JSV · 5 publications · 133 citations

    5

    h-index

1–5