Subsonic Combustion

Subsonic Combustion is a combustion process in which the airflow within the combustion chamber of a ramjet engine remains below sonic speed, distinguishing it from supersonic combustion by enabling flame stabilization through lower velocity, diffusion-controlled mixing and reaction in a decelerated, compressed inlet flow.

153

Publications

5.2K

Citations

406

Authors

156

Institutions

Publications per year

2017–2026

21

Authors

406

  1. KS
    K. SCHADOW

    Naval Air Warfare Center Weapons Division, United States

    7 publications · 240 citations

    7

    h-index

  2. KK
    Kenji Kudo

    Japan Aerospace Exploration Agency, Japan

    7 publications · 306 citations

    7

    h-index

  3. AM
    Atsuo Murakami

    Japan Aerospace Exploration Agency, Japan

    5 publications · 148 citations

    5

    h-index

  4. EG
    Ephraim Gutmark

    University of Cincinnati, United States

    5 publications · 206 citations

    5

    h-index

  5. TK
    Takeshi Kanda

    Japan Aerospace Exploration Agency, Japan

    4 publications · 180 citations

    4

    h-index

1–5 of 406

Venues

  1. Journal of Propulsion and Power

    22 publications · 992 citations

    16

    h-index

  2. AIAA Journal

    10 publications · 304 citations

    10

    h-index

  3. Combustion Science and Technology

    CST · 4 publications · 113 citations

    4

    h-index

  4. 4

    h-index

  5. Physics of Fluids

    4 publications · 195 citations

    4

    h-index

1–5