Trailing-edge Design

Trailing-Edge Design is a method in airfoil theory that specifies the geometric and aerodynamic configuration of the aftmost region of an airfoil to optimize flow attachment, minimize drag, and control vortex shedding at the boundary layer exit.

115

Publications

4K

Citations

338

Authors

126

Institutions

Publications per year

2017–2026

41

Authors

338

  1. FA
    Francesco Avallone

    Delft University of Technology, Netherlands

    5 publications · 181 citations

    5

    h-index

  2. MH
    Michaela Herr

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

    5 publications · 313 citations

    5

    h-index

  3. DR
    Daniele Ragni

    Delft University of Technology, Netherlands

    5 publications · 181 citations

    5

    h-index

  4. AC
    Antonio Concilio

    Italian Aerospace Research Centre, Italy

    4 publications · 176 citations

    4

    h-index

  5. JR
    Joaquim R. R. A. Martins

    University of Michigan, United States

    4 publications · 177 citations

    4

    h-index

1–5 of 338

Venues

  1. Aerospace Science and Technology

    AST · 7 publications · 261 citations

    7

    h-index

  2. Journal of Aircraft

    6 publications · 130 citations

    6

    h-index

  3. Journal of Sound and Vibration

    JSV · 5 publications · 185 citations

    5

    h-index

  4. Applied Acoustics

    3 publications · 133 citations

    4

    h-index

  5. AIAA Journal

    4 publications · 291 citations

    4

    h-index

1–5