Blade Flutter

Blade Flutter is a self-excited aeroelastic instability characterized by sustained or divergent oscillations of a rotor blade resulting from the coupled interaction between aerodynamic, elastic, and inertial forces under specific flow conditions.

196

Publications

7.1K

Citations

376

Authors

145

Institutions

Publications per year

2017–2026

48

Authors

376

  1. RE
    Robert E. Kielb

    Duke University, United States

    12 publications · 435 citations

    12

    h-index

  2. KR
    K. R. V. Kaza

    Glenn Research Center, United States

    8 publications · 259 citations

    8

    h-index

  3. OM
    Oral Mehmed

    Glenn Research Center, United States

    6 publications · 146 citations

    6

    h-index

  4. DS
    D. S. Whitehead

    Bridge University, South Sudan

    6 publications · 398 citations

    6

    h-index

  5. LH
    L. He

    University of Oxford, United Kingdom

    5 publications · 107 citations

    5

    h-index

1–5 of 376

Venues

  1. Journal of Turbomachinery

    25 publications · 688 citations

    16

    h-index

  2. 11

    h-index

  3. Journal of Fluids and Structures

    7 publications · 421 citations

    7

    h-index

  4. AIAA Journal

    7 publications · 254 citations

    7

    h-index

  5. Journal of the American Helicopter Society

    6 publications · 207 citations

    6

    h-index

1–5