Mach Number Effects

Mach Number Effects is a theoretical construct in aerodynamics that characterizes the distinct influence of the ratio of flow velocity to the local speed of sound on compressible flow behavior, control surface dynamics, cruise performance, and propulsion efficiency in ramjet engines.

2.7K

Publications

113.4K

Citations

5.4K

Authors

1.2K

Institutions

Publications per year

2017–2026

433

Authors

5.4K

  1. SA
    Sher Afghan Khan

    International Islamic University Malaysia, Malaysia

    31 publications · 718 citations

    16

    h-index

  2. MS
    M. S. Howe

    Boston University, United States

    15 publications · 1.1K citations

    15

    h-index

  3. CT
    C. T. Russell

    University of California, Los Angeles, United States

    15 publications · 1K citations

    15

    h-index

  4. CB
    Christophe Bogey

    Laboratoire de Mécanique des Fluides et d'Acoustique, France

    14 publications · 550 citations

    14

    h-index

  5. MS
    Mo Samimy

    The Ohio State University, United States

    15 publications · 1.2K citations

    13

    h-index

1–5 of 5.4K

Venues

  1. Journal of Fluid Mechanics

    179 publications · 14.6K citations

    62

    h-index

  2. AIAA Journal

    232 publications · 11.8K citations

    56

    h-index

  3. Physics of Fluids

    90 publications · 3.2K citations

    34

    h-index

  4. The Astrophysical Journal

    ApJ · 57 publications · 3.2K citations

    32

    h-index

  5. Physics of Plasmas

    65 publications · 3K citations

    31

    h-index

1–5