Variable Geometry Inlets

Variable Geometry Inlets is a type of airbreathing engine inlet system designed for high-speed propulsion that dynamically adjusts its geometric configuration to optimize airflow compression and pressure recovery across varying flight Mach numbers, particularly in ramjet and scramjet engines.

31

Publications

1K

Citations

93

Authors

29

Institutions

Publications per year

2017–2026

8

Authors

93

  1. ZD
    Zhengtao Ding

    University of Manchester, United Kingdom

    3 publications · 83 citations

    3

    h-index

  2. LD
    Liqian Dou

    Tianjin University, China

    3 publications · 83 citations

    3

    h-index

  3. QZ
    Qun Zong

    Tianjin University, China

    2 publications · 44 citations

    2

    h-index

  4. PS
    Peihua Su

    Tianjin University, China

    2 publications · 69 citations

    2

    h-index

  5. JS
    João Soares

    Universidade do Porto, Portugal

    1 publications · 65 citations

    1

    h-index

1–5 of 93

Venues

  1. Aerospace Science and Technology

    AST · 6 publications · 190 citations

    6

    h-index

  2. Energy Conversion and Management

    2 publications · 120 citations

    2

    h-index

  3. Journal of Propulsion and Power

    2 publications · 84 citations

    2

    h-index

  4. Journal of the Franklin Institute

    1 publications · 14 citations

    1

    h-index

  5. 37th Aerospace Sciences Meeting and Exhibit

    1 publications · 10 citations

    1

    h-index

1–5