Flow Unstart Phenomena

Flow Unstart Phenomena is a transient aerodynamic instability in supersonic combustion systems, characterized by the abrupt detachment of the terminal shock wave from the inlet, leading to a breakdown of stable supersonic flow and resulting in a sudden loss of engine performance.

104

Publications

4.9K

Citations

253

Authors

80

Institutions

Publications per year

2017–2026

25

Variants

Inlet Unstart

Authors

253

  1. WB
    Wen Bao

    Harbin Institute of Technology, China

    9 publications · 502 citations

    9

    h-index

  2. NT
    Noel T. Clemens

    The University of Texas at Austin, United States

    8 publications · 572 citations

    8

    h-index

  3. JL
    Justin L. Wagner

    Sandia National Laboratories, United States

    8 publications · 661 citations

    8

    h-index

  4. JC
    Juntao Chang

    Harbin Institute of Technology, China

    8 publications · 489 citations

    8

    h-index

  5. HT
    Huijun Tan

    Nanjing University of Aeronautics and Astronautics, China

    7 publications · 527 citations

    7

    h-index

1–5 of 253

Venues

  1. Journal of Propulsion and Power

    16 publications · 908 citations

    15

    h-index

  2. AIAA Journal

    12 publications · 982 citations

    11

    h-index

  3. Aerospace Science and Technology

    AST · 7 publications · 191 citations

    7

    h-index

  4. The Aeronautical Journal

    5 publications · 134 citations

    5

    h-index

  5. Physics of Fluids

    3 publications · 112 citations

    3

    h-index

1–5