Variable-cycle Hypersonic Engines

Variable-Cycle Hypersonic Engines is a type of air-breathing propulsion system that integrates multiple thermodynamic cycles within a single engine architecture to enable efficient and stable operation across a wide range of flight Mach numbers, particularly transitioning seamlessly from supersonic to hypersonic speeds by adaptively modulating airflow pathways and combustion modes.

11

Publications

405

Citations

24

Authors

14

Institutions

Publications per year

2017–2026

1

Variants

Variable Cycle Hypersonic Engines

Authors

24

  1. SA
    S. Adibhatla

    General Electric (United States), United States

    4 publications · 148 citations

    4

    h-index

  2. MC
    Min Chen

    Beihang University, China

    2 publications · 54 citations

    2

    h-index

  3. SG
    Sanjay Garg

    University of South Australia, Australia

    2 publications · 99 citations

    2

    h-index

  4. YW
    Yanjun Wang

    Nanjing University of Aeronautics and Astronautics, China

    1 publications · 43 citations

    1

    h-index

  5. DF
    D.K. Frederick

    Rensselaer Polytechnic Institute, United States

    1 publications · 85 citations

    1

    h-index

1–5 of 24

Venues

  1. OhioLink ETD Center (Ohio Library and Information Network)

    Repository · 1 publications · 66 citations

    1

    h-index

  2. 32nd Joint Propulsion Conference and Exhibit

    Conference · 1 publications · 14 citations

    1

    h-index

  3. 1

    h-index

  4. Progress in Aerospace Sciences

    1 publications · 78 citations

    1

    h-index

  5. 1

    h-index

1–5