Concepedia

Asymmetric Stall

Asymmetric Stall is a stall dynamics phenomenon characterized by the unequal onset of flow separation and loss of lift between the two wings or sides of an aircraft, leading to uncommanded roll or yaw due to disparate aerodynamic performance across the span.

2

Publications

141

Citations

6

Authors

4

Institutions

Publications per year

2017–2026

0

Parents

Publications

2

1–2 of 2

Authors

6

  1. YT
    Yoshinobu TSUJIMOTO

    The University of Osaka, Japan

    2 publications · 141 citations

    2

    h-index

  2. YN
    Yuki Nakamura

    The University of Tokyo, Japan

    2 publications · 141 citations

    2

    h-index

  3. YY
    Yoshiki YOSHIDA

    The University of Osaka, Japan

    2 publications · 141 citations

    2

    h-index

  4. TM
    Tatsuhito Matsushima

    Takasago (Japan), Japan

    1 publications · 88 citations

    1

    h-index

  5. TS
    Takeshi Sano

    Sanyo (Japan), Japan

    1 publications · 88 citations

    1

    h-index

1–5 of 6

Institutions

4

  1. Takasago (Japan)

    Tokyo, Japan

    2 h-index

    4 publications

    282 citations

  2. The University of Osaka

    Osaka, Japan

    2 h-index

    4 publications

    282 citations

  3. Mitsubishi Heavy Industries (Germany)

    Munich, Germany

    1 h-index

    2 publications

    106 citations

  4. Mitsubishi Heavy Industries (Japan)

    Tokyo, Japan

    1 h-index

    2 publications

    176 citations

1–4 of 4

Venues

  1. JSME International Journal Series B

    1 publications · 53 citations

    1

    h-index

  2. Journal of Fluids Engineering

    1 publications · 88 citations

    1

    h-index

1–2