Control Surface Deflection Effects

Control Surface Deflection Effects is a mechanical aerodynamic phenomenon denoting the alterations in aerodynamic forces and moments on an aircraft resulting from the angular displacement of control surfaces relative to the airflow, distinguished by its direct influence on the vehicle's stability and maneuverability.

15

Publications

636

Citations

39

Authors

16

Institutions

Publications per year

2017–2026

2

Authors

39

  1. PD
    Philippe Dépincé

    Centre National de la Recherche Scientifique, France

    2 publications · 161 citations

    2

    h-index

  2. JH
    Jean-Yves Hascoët

    Centre National de la Recherche Scientifique, France

    2 publications · 161 citations

    2

    h-index

  3. GP
    Guru P. Guruswamy

    Ames Research Center, United States

    1 publications · 17 citations

    1

    h-index

  4. KL
    Keh Lih Tzuoo

    Nielsen Engineering & Research (United States), United States

    1 publications · 19 citations

    1

    h-index

  5. MW
    Michael W. Oppenheimer

    United States Air Force Research Laboratory, United States

    1 publications · 26 citations

    1

    h-index

1–5 of 39

Venues

  1. Journal of Aircraft

    4 publications · 105 citations

    4

    h-index

  2. 2

    h-index

  3. AIAA Journal

    1 publications · 67 citations

    1

    h-index

  4. KSME International Journal

    1 publications · 17 citations

    1

    h-index

  5. AIAA Guidance, Navigation and Control Conference and Exhibit

    Conference · 1 publications · 26 citations

    1

    h-index

1–5