Combustor Geometry

Combustor Geometry is a structural design specification that defines the physical configuration and dimensional characteristics of the combustion chamber in a scramjet engine, distinguishing it from other propulsion system components by its direct influence on supersonic airflow, fuel mixing efficiency, and thermal management within the context of hypersonic flight.

722

Publications

27.8K

Citations

1.9K

Authors

425

Institutions

Publications per year

2017–2026

323

Authors

1.9K

  1. MS
    Mingbo Sun

    National University of Defense Technology, China

    26 publications · 1.3K citations

    21

    h-index

  2. EJ
    E Jiaqiang

    Hunan University, China

    18 publications · 1.2K citations

    17

    h-index

  3. WB
    Wen Bao

    Harbin Institute of Technology, China

    22 publications · 1.1K citations

    17

    h-index

  4. KM
    Krishna Murari Pandey

    National Institute Of Technology Silchar, India

    20 publications · 1.1K citations

    16

    h-index

  5. JC
    Juntao Chang

    Harbin Institute of Technology, China

    20 publications · 1.1K citations

    16

    h-index

1–5 of 1.9K

Venues

  1. International Journal of Hydrogen Energy

    70 publications · 3.7K citations

    36

    h-index

  2. Aerospace Science and Technology

    AST · 57 publications · 1.9K citations

    30

    h-index

  3. Energy

    39 publications · 1.7K citations

    27

    h-index

  4. Applied Thermal Engineering

    37 publications · 1.7K citations

    27

    h-index

  5. Acta Astronautica

    36 publications · 1.6K citations

    25

    h-index

1–5