Transonic Boundary Layers

Transonic Boundary Layers is a fluid dynamic phenomenon characterized as a thin viscous region adjacent to a solid surface wherein the flow transitions through Mach numbers near unity, distinguished by the coexistence of subsonic and supersonic regions, strong adverse pressure gradients, and shock wave-boundary layer interactions that critically influence aerodynamic performance and flow separation behavior.

88

Publications

3.6K

Citations

175

Authors

83

Institutions

Publications per year

2017–2026

9

Authors

175

  1. CS
    Cathleen S. Morawetz

    Courant Institute of Mathematical Sciences, United States

    5 publications · 451 citations

    5

    h-index

  2. FT
    F. T. Smith

    University College London, United Kingdom

    3 publications · 158 citations

    3

    h-index

  3. LQ
    Lei Qiao

    Northwestern Polytechnical University, China

    2 publications · 125 citations

    3

    h-index

  4. JX
    Jiakuan Xu

    Northwestern Polytechnical University, China

    2 publications · 125 citations

    3

    h-index

  5. GR
    G. R. Inger

    Iowa State University, United States

    3 publications · 60 citations

    3

    h-index

1–5 of 175

Venues

  1. AIAA Journal

    19 publications · 533 citations

    15

    h-index

  2. Communications on Pure and Applied Mathematics

    7 publications · 456 citations

    7

    h-index

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

    Repository · 3 publications · 124 citations

    3

    h-index

  4. Physics of Fluids

    3 publications · 58 citations

    3

    h-index

  5. Computers & Fluids

    3 publications · 98 citations

    3

    h-index

1–5