Flutter Boundary Determination

Flutter Boundary Determination is a methodological construct in aeroelastic testing that identifies the critical combination of flight conditions, such as airspeed and altitude, at which a structure transitions from stable oscillatory behavior to unstable, self-sustaining oscillations due to aerodynamic, elastic, and inertial coupling.

80

Publications

2.5K

Citations

196

Authors

85

Institutions

Publications per year

2017–2026

19

Authors

196

  1. PB
    Philip Beran

    United States Air Force Research Laboratory, United States

    5 publications · 116 citations

    5

    h-index

  2. MV
    Mehdi Vahdati

    Imperial College London, United Kingdom

    4 publications · 138 citations

    4

    h-index

  3. UR
    Ulf Ringertz

    KTH Royal Institute of Technology, Sweden

    2 publications · 43 citations

    2

    h-index

  4. KL
    Kuen-Bae Lee

    Rolls-Royce (United Kingdom), United Kingdom

    2 publications · 60 citations

    2

    h-index

  5. DB
    Dan Borglund

    KTH Royal Institute of Technology, Sweden

    2 publications · 43 citations

    2

    h-index

1–5 of 196

Venues

  1. AIAA Journal

    15 publications · 518 citations

    12

    h-index

  2. Journal of Aircraft

    11 publications · 586 citations

    11

    h-index

  3. 4

    h-index

  4. Journal of Guidance Control and Dynamics

    4 publications · 111 citations

    4

    h-index

  5. Journal of Turbomachinery

    4 publications · 136 citations

    4

    h-index

1–5