Engine Matching

Engine Matching is a methodological framework in aerospace engineering that systematically aligns the performance characteristics of gas turbine engines—such as thrust, specific fuel consumption, and operability limits—with the aerodynamic, mission, and design requirements of an aircraft to ensure optimal integration and efficiency across operational regimes.

31

Publications

845

Citations

80

Authors

31

Institutions

Publications per year

2017–2026

17

Authors

80

  1. GZ
    Guangmeng Zhou

    Academy of Military Transportation, China

    2 publications · 35 citations

    2

    h-index

  2. RL
    Ruilin Liu

    Academy of Military Transportation, China

    2 publications · 35 citations

    2

    h-index

  3. SE
    Selçuk Ekici

    Iğdır Üniversitesi, Türkiye

    2 publications · 56 citations

    2

    h-index

  4. FL
    Feng-yu Lai

    Beijing Institute of Technology, China

    1 publications · 19 citations

    2

    h-index

  5. YJ
    Yufei Jiao

    Naval University of Engineering, China

    2 publications · 35 citations

    2

    h-index

1–5 of 80

Venues

  1. 3

    h-index

  2. 2

    h-index

  3. Chinese Journal of Aeronautics

    CJA · 2 publications · 127 citations

    2

    h-index

  4. International Journal of Engine Research

    2 publications · 26 citations

    2

    h-index

  5. Journal of Power and Energy Engineering

    JPEE · 2 publications · 34 citations

    2

    h-index

1–5