Vortex Ring State

Vortex Ring State is a hazardous aerodynamic condition in rotorcraft flight dynamics, characterized by the ingestion of recirculating wake vortices into the rotor disk, resulting in a self-sustaining flow regime that induces significant lift loss and uncommanded descent despite positive rotor pitch.

176

Publications

8.6K

Citations

547

Authors

246

Institutions

Publications per year

2017–2026

27

Variants

Settling With Power

Authors

547

  1. KM
    Kazumi Maki

    University of Southern California, United States

    6 publications · 146 citations

    6

    h-index

  2. CA
    C. A. Ross

    Massachusetts Institute of Technology, United States

    6 publications · 169 citations

    6

    h-index

  3. HJ
    Hyung Jin Won

    University of Ulsan, South Korea

    5 publications · 122 citations

    5

    h-index

  4. FM
    F. M. Peeters

    University of Antwerp, Belgium

    5 publications · 433 citations

    5

    h-index

  5. FC
    Fernando Castaño

    University of the Basque Country, Spain

    5 publications · 166 citations

    5

    h-index

1–5 of 547

Venues

  1. Physical Review Letters

    PRL · 15 publications · 933 citations

    15

    h-index

  2. Applied Physics Letters

    13 publications · 593 citations

    13

    h-index

  3. Journal of Applied Physics

    8 publications · 181 citations

    8

    h-index

  4. Physica C Superconductivity

    8 publications · 128 citations

    8

    h-index

  5. Journal of the American Helicopter Society

    6 publications · 195 citations

    6

    h-index

1–5