Tip Vortex Reduction

Tip Vortex Reduction is a methodological construct in propeller design that specifically addresses the mitigation of vortical flow structures generated at blade tips by altering blade geometry or flow conditions to minimize energy loss and improve hydrodynamic or aerodynamic efficiency.

99

Publications

2.9K

Citations

260

Authors

103

Institutions

Publications per year

2017–2026

36

Authors

260

  1. CZ
    Chao Zhou

    Peking University, China

    7 publications · 268 citations

    7

    h-index

  2. QZ
    Qun Zheng

    Harbin Engineering University, China

    4 publications · 92 citations

    4

    h-index

  3. JK
    Joseph Katz

    Johns Hopkins University, United States

    4 publications · 65 citations

    4

    h-index

  4. RP
    Richard P. Woodward

    Glenn Research Center, United States

    3 publications · 57 citations

    3

    h-index

  5. HC
    Huang Chen

    Johns Hopkins University, United States

    3 publications · 48 citations

    3

    h-index

1–5 of 260

Venues

  1. Journal of Turbomachinery

    7 publications · 304 citations

    7

    h-index

  2. Journal of Aircraft

    6 publications · 229 citations

    6

    h-index

  3. Journal of Fluids Engineering

    5 publications · 232 citations

    5

    h-index

  4. Ocean Engineering

    5 publications · 156 citations

    5

    h-index

  5. Aerospace Science and Technology

    AST · 5 publications · 232 citations

    5

    h-index

1–5