Dynamic Stall

Dynamic Stall is a transient aerodynamic phenomenon characterized by the delayed separation of airflow and the subsequent cyclic formation and shedding of leading-edge vortices on lifting surfaces undergoing unsteady motion, distinguishing it from steady stall by its dependence on flow inertia and time-dependent angle-of-attack variations.

807

Publications

38.6K

Citations

1.4K

Authors

396

Institutions

Publications per year

2017–2026

231

Authors

1.4K

  1. MR
    Miguel R. Visbal

    United States Air Force Research Laboratory, United States

    38 publications · 1.7K citations

    24

    h-index

  2. LW
    L. W. Carr

    Ames Research Center, United States

    30 publications · 3K citations

    22

    h-index

  3. MS
    M. S. Chandrasekhara

    Naval Postgraduate School, United States

    28 publications · 954 citations

    18

    h-index

  4. WJ
    W. J. Mccroskey

    Ames Research Center, United States

    17 publications · 2.1K citations

    16

    h-index

  5. DG
    David Greenblatt

    Technion – Israel Institute of Technology, Israel

    17 publications · 876 citations

    15

    h-index

1–5 of 1.4K

Venues

  1. AIAA Journal

    104 publications · 6K citations

    44

    h-index

  2. Journal of Aircraft

    73 publications · 3.7K citations

    34

    h-index

  3. Wind Energy

    35 publications · 2K citations

    25

    h-index

  4. Journal of the American Helicopter Society

    40 publications · 2.5K citations

    25

    h-index

  5. Physics of Fluids

    22 publications · 739 citations

    18

    h-index

1–5