Stall-spin Entry

Stall-Spin Entry is a critical flight dynamic event characterized by the transition from controlled flight to an uncontrolled rotational departure, initiated by an aerodynamic stall that leads to autorotation about the aircraft’s vertical axis, within the context of lateral-directional stability and control.

13

Publications

239

Citations

23

Authors

11

Institutions

Publications per year

2017–2026

0

Authors

23

  1. SB
    S. B. Anderson

    Ames Research Center, United States

    2 publications · 42 citations

    2

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  2. IK
    Ilan Kroo

    Stanford University, United States

    2 publications · 30 citations

    2

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  3. AR
    Adam Ragheb

    University of Illinois Urbana-Champaign, United States

    2 publications · 39 citations

    2

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  4. RA
    R. A. Kroeger

    United States Naval Research Laboratory, United States

    2 publications · 34 citations

    2

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  5. OD
    Or D. Dantsker

    University of Illinois Urbana-Champaign, United States

    2 publications · 39 citations

    2

    h-index

1–5 of 23

Venues

  1. Journal of Aircraft

    2 publications · 37 citations

    2

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  2. 31st AIAA Applied Aerodynamics Conference

    Conference · 2 publications · 39 citations

    2

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  3. 2

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  4. Aerospace Science and Technology

    AST · 1 publications · 37 citations

    1

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  5. AIAA Atmospheric Flight Mechanics Conference

    Conference · 1 publications · 18 citations

    1

    h-index

1–5