Wing Configuration Design

Wing Configuration Design is a methodological framework within aircraft configuration design that specifically governs the determination of geometric, aerodynamic, and structural parameters of a wing to achieve optimal performance, stability, and integration with the overall aircraft architecture.

135

Publications

4.5K

Citations

388

Authors

128

Institutions

Publications per year

2017–2026

36

Authors

388

  1. RT
    Raphael T. Haftka

    University of Florida, United States

    3 publications · 94 citations

    3

    h-index

  2. RN
    R Nangia

    Applied Research Associates, New Zealand

    3 publications · 57 citations

    3

    h-index

  3. JA
    Joseph A. Schetz

    Virginia Tech, United States

    3 publications · 106 citations

    3

    h-index

  4. CM
    Carsten M. Liersch

    Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR), Germany

    3 publications · 95 citations

    3

    h-index

  5. DN
    Dimitri N. Mavris

    Georgia Institute of Technology, United States

    3 publications · 62 citations

    3

    h-index

1–5 of 388

Venues

  1. Journal of Aircraft

    15 publications · 453 citations

    13

    h-index

  2. 6

    h-index

  3. Aerospace Science and Technology

    AST · 6 publications · 172 citations

    6

    h-index

  4. NASA STI Repository (National Aeronautics and Space Administration)

    Repository · 4 publications · 101 citations

    4

    h-index

  5. 2018 Applied Aerodynamics Conference

    Conference · 3 publications · 54 citations

    3

    h-index

1–5