Variable Geometry Engines

Variable Geometry Engines is a class of air-breathing propulsion systems in which the physical configuration of key engine components, such as inlet ducts, compressor blades, or exhaust nozzles, can be actively adjusted during operation to optimize performance across varying flight conditions and engine regimes.

64

Publications

2.1K

Citations

204

Authors

79

Institutions

Publications per year

2017–2026

14

Authors

204

  1. MB
    Marc Bouchez

    MBDA (France), France

    4 publications · 80 citations

    4

    h-index

  2. VA
    Valery Avrashkov

    Moscow Aviation Institute, Russia

    4 publications · 80 citations

    4

    h-index

  3. CC
    Changpeng Cai

    Nanjing University of Aeronautics and Astronautics, China

    3 publications · 91 citations

    3

    h-index

  4. QZ
    Qiangang Zheng

    Nanjing University of Aeronautics and Astronautics, China

    3 publications · 91 citations

    3

    h-index

  5. IK
    Ilya Kolmanovsky

    University of Michigan, United States

    3 publications · 396 citations

    3

    h-index

1–5 of 204

Venues

  1. 10

    h-index

  2. Aerospace Science and Technology

    AST · 3 publications · 99 citations

    3

    h-index

  3. Journal of Aircraft

    3 publications · 37 citations

    3

    h-index

  4. Applied Thermal Engineering

    3 publications · 72 citations

    3

    h-index

  5. Journal of Turbomachinery

    2 publications · 59 citations

    2

    h-index

1–5