Prandtl-meyer Flow

Prandtl-Meyer Flow is a theoretical model in supersonic aerodynamics that describes the isentropic expansion of a supersonic flow around a convex corner, characterized by a continuous fan of expansion waves that increase the flow Mach number while decreasing pressure and density.

42

Publications

1.7K

Citations

73

Authors

48

Institutions

Publications per year

2017–2026

4

Authors

73

  1. MW
    Michael W. Oppenheimer

    United States Air Force Research Laboratory, United States

    2 publications · 146 citations

    2

    h-index

  2. GC
    Gui‐Qiang Chen

    Northwestern University, United States

    2 publications · 33 citations

    2

    h-index

  3. DD
    David Doman

    United States Air Force Research Laboratory, United States

    2 publications · 146 citations

    2

    h-index

  4. MB
    Myoungjean Bae

    Pohang University of Science and Technology, South Korea

    2 publications · 33 citations

    2

    h-index

  5. TZ
    Toufik Zebbiche

    University of Blida, Algeria

    2 publications · 41 citations

    2

    h-index

1–5 of 73

Venues

  1. AIAA Journal

    9 publications · 193 citations

    9

    h-index

  2. Journal of Fluid Mechanics

    5 publications · 205 citations

    5

    h-index

  3. The Physics of Fluids

    5 publications · 403 citations

    5

    h-index

  4. Physical Review

    2 publications · 78 citations

    2

    h-index

  5. AIAA Atmospheric Flight Mechanics Conference and Exhibit

    Conference · 2 publications · 146 citations

    2

    h-index

1–5