Injector Impingement

Injector impingement is a combustion process in liquid rocket engines wherein propellant streams are deliberately directed to collide at specified angles and velocities, enhancing atomization and mixing efficiency to stabilize ignition and improve combustion performance.

72

Publications

2.5K

Citations

241

Authors

76

Institutions

Publications per year

2017–2026

24

Authors

241

  1. LY
    Lijun Yang

    Beihang University, China

    3 publications · 106 citations

    3

    h-index

  2. TH
    Takehiro Himeno

    The University of Tokyo, Japan

    3 publications · 40 citations

    3

    h-index

  3. TW
    Thomas Wallner

    Argonne National Laboratory, United States

    3 publications · 127 citations

    3

    h-index

  4. CI
    Chihiro Inoue

    Kyushu University, Japan

    3 publications · 40 citations

    3

    h-index

  5. TW
    Toshinori Watanabe

    The University of Tokyo, Japan

    3 publications · 40 citations

    3

    h-index

1–5 of 241

Venues

  1. 10

    h-index

  2. Journal of Propulsion and Power

    7 publications · 201 citations

    7

    h-index

  3. Fuel

    4 publications · 163 citations

    4

    h-index

  4. Aerospace Science and Technology

    AST · 3 publications · 89 citations

    3

    h-index

  5. Atomization and Sprays

    3 publications · 55 citations

    3

    h-index

1–5