Concepedia

V-tail Configuration

V-Tail Configuration is an aircraft empennage design in which the traditional horizontal and vertical tail surfaces are replaced by two inclined tail surfaces arranged in a V-shaped arrangement, thereby combining pitch and yaw control functions into a single integrated structure.

2

Publications

57

Citations

11

Authors

2

Institutions

Publications per year

2017–2026

2

Variants

V-tailV-tail Empennage

Parents

Publications

2

1–2 of 2

Authors

11

  1. FQ
    Fuxiang Qiao

    Northwestern Polytechnical University, China

    1 publications · 32 citations

    1

    h-index

  2. AO
    Anı́bal Ollero

    Universidad de Sevilla, Spain

    1 publications · 25 citations

    1

    h-index

  3. RZ
    Raphael Zufferey

    Imperial College London, United Kingdom

    1 publications · 25 citations

    1

    h-index

  4. JS
    Jingping Shi

    Northwestern Polytechnical University, China

    1 publications · 32 citations

    1

    h-index

  5. YL
    Yongxi Lyu

    Northwestern Polytechnical University, China

    1 publications · 32 citations

    1

    h-index

1–5 of 11

Institutions

2

  1. Northwestern Polytechnical University

    Xi'an, China

    1 h-index

    4 publications

    128 citations

  2. Universidad de Sevilla

    Seville, Spain

    1 h-index

    7 publications

    175 citations

1–2 of 2

Venues

  1. 1

    h-index

  2. 1

    h-index

1–2