Leading-edge Design

Leading-Edge Design is an aerodynamic configuration principle within airfoil theory for fixed-pitch propellers that specifies the geometry and curvature of the forwardmost section of the blade to optimize stall characteristics, pressure distribution, and flow attachment under operational conditions.

203

Publications

11K

Citations

567

Authors

182

Institutions

Publications per year

2017–2026

68

Authors

567

  1. PJ
    Phillip Joseph

    University of Southampton, United Kingdom

    5 publications · 146 citations

    5

    h-index

  2. AB
    Andrew B. Kahng

    University of California San Diego, United States

    5 publications · 298 citations

    5

    h-index

  3. MB
    Michael Bragg

    University of Illinois Urbana-Champaign, United States

    4 publications · 80 citations

    4

    h-index

  4. DV
    D. V. Maddalon

    Langley Research Center, United States

    3 publications · 69 citations

    4

    h-index

  5. PC
    Paruchuri Chaitanya

    University of Southampton, United Kingdom

    4 publications · 126 citations

    4

    h-index

1–5 of 567

Venues

  1. Journal of Aircraft

    14 publications · 632 citations

    12

    h-index

  2. NASA Technical Reports Server (NASA)

    Repository · 6 publications · 121 citations

    7

    h-index

  3. Journal of Turbomachinery

    6 publications · 282 citations

    6

    h-index

  4. Aerospace Science and Technology

    AST · 6 publications · 156 citations

    6

    h-index

  5. Ocean Engineering

    4 publications · 85 citations

    5

    h-index

1–5