Empennage Configuration

Empennage Configuration is a structural design framework in aerospace engineering that specifies the arrangement and orientation of an aircraft's tail surfaces, distinguishing it from other airframe configurations by its role in providing stability and control about the pitch and yaw axes.

7

Publications

107

Citations

19

Authors

9

Institutions

Publications per year

2017–2026

4

Variants

Tail Configuration

Authors

19

  1. MM
    Mauro Minervino

    Italian Aerospace Research Centre, Italy

    1 publications · 16 citations

    1

    h-index

  2. JF
    John F. Kennedy

    Trinity College Dublin, Ireland

    1 publications · 16 citations

    1

    h-index

  3. JE
    Julio Enoc Parra Villamarín

    Fundación Universitaria Los Libertadores, Colombia

    1 publications · 30 citations

    1

    h-index

  4. DF
    David Findlay

    United States Navy, United States

    2 publications · 26 citations

    1

    h-index

  5. SC
    Salvatore Corcione

    University of Naples Federico II, Italy

    1 publications · 11 citations

    1

    h-index

1–5 of 19

Venues

  1. Aerospace

    2 publications · 21 citations

    2

    h-index

  2. International Journal of Aeroacoustics

    1 publications · 16 citations

    1

    h-index

  3. MATEC Web of Conferences

    1 publications · 13 citations

    1

    h-index

  4. 35th Aerospace Sciences Meeting and Exhibit

    1 publications · 13 citations

    1

    h-index

  5. 1

    h-index

1–5