Supersonic Boundary Layers

Supersonic Boundary Layers is a type of boundary-layer flow characterized by the presence of supersonic velocities within the boundary layer, distinguished from subsonic boundary layers by the occurrence of compressibility effects, shock waves, and thermal gradients resulting from high-speed external flow exceeding the speed of sound.

746

Publications

32.4K

Citations

1.2K

Authors

319

Institutions

Publications per year

2017–2026

136

Authors

1.2K

  1. AJ
    Alexander J. Smits

    Princeton University, United States

    21 publications · 1.2K citations

    17

    h-index

  2. YZ
    Yuxin Zhao

    National University of Defense Technology, China

    16 publications · 516 citations

    15

    h-index

  3. SY
    Shihe Yi

    National University of Defense Technology, China

    18 publications · 481 citations

    15

    h-index

  4. LH
    Lin He

    National University of Defense Technology, China

    11 publications · 332 citations

    11

    h-index

  5. MR
    Mujeeb R. Malik

    Science and Technology Corporation (United States), United States

    10 publications · 884 citations

    10

    h-index

1–5 of 1.2K

Venues

  1. Journal of Fluid Mechanics

    88 publications · 7.2K citations

    46

    h-index

  2. AIAA Journal

    127 publications · 6.6K citations

    43

    h-index

  3. Physics of Fluids

    45 publications · 2.9K citations

    27

    h-index

  4. Fluid Dynamics

    21 publications · 515 citations

    14

    h-index

  5. Aerospace Science and Technology

    AST · 13 publications · 256 citations

    12

    h-index

1–5