Static Stall

Static Stall is a theoretical construct in aerodynamics that defines the critical angle of attack at which airflow separation occurs over a stationary airfoil, resulting in a sudden loss of lift due to the breakdown of attached flow under steady-state conditions.

47

Publications

2K

Citations

138

Authors

56

Institutions

Publications per year

2017–2026

11

Authors

138

  1. SS
    Scott Schreck

    National Laboratory of the Rockies, United States

    4 publications · 141 citations

    4

    h-index

  2. WE
    William E. Faller

    Johns Hopkins University, United States

    4 publications · 141 citations

    4

    h-index

  3. MO
    Michael Ol

    United States Air Force Research Laboratory, United States

    2 publications · 126 citations

    2

    h-index

  4. DP
    Donald P. Rizzetta

    United States Air Force Research Laboratory, United States

    2 publications · 78 citations

    2

    h-index

  5. AG
    Anthony Gardner

    Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR), Germany

    2 publications · 55 citations

    2

    h-index

1–5 of 138

Venues

  1. Journal of Aircraft

    7 publications · 165 citations

    7

    h-index

  2. AIAA Journal

    6 publications · 289 citations

    6

    h-index

  3. Physics of Fluids

    3 publications · 208 citations

    3

    h-index

  4. Journal of Fluids Engineering

    2 publications · 126 citations

    2

    h-index

  5. Wind Energy

    2 publications · 52 citations

    2

    h-index

1–5