Variable Geometry Nozzles

Variable Geometry Nozzles is a specialized type of propulsion nozzle system that belongs to the class of aerospace flow control devices, distinguished by its ability to dynamically alter geometric parameters such as throat area, exit area, or contour in response to varying flight conditions to optimize thrust and engine performance across operational regimes.

53

Publications

1.5K

Citations

180

Authors

74

Institutions

Publications per year

2017–2026

17

Authors

180

  1. CK
    Ching-Wen Kuo

    Pennsylvania State University, United States

    3 publications · 106 citations

    3

    h-index

  2. TK
    Takayuki Kojima

    Japan Aerospace Exploration Agency, Japan

    2 publications · 42 citations

    2

    h-index

  3. NR
    Nancy Rey

    Hartford Financial Services (United States)

    2 publications · 36 citations

    2

    h-index

  4. DB
    Dan Baruzzini

    Lockheed Martin (Canada), Canada

    2 publications · 25 citations

    2

    h-index

  5. KK
    Kursat Kara

    Oklahoma State University, United States

    2 publications · 37 citations

    2

    h-index

1–5 of 180

Venues

  1. Applied Thermal Engineering

    7 publications · 305 citations

    7

    h-index

  2. International Journal of Aeroacoustics

    3 publications · 96 citations

    3

    h-index

  3. Aerospace Science and Technology

    AST · 3 publications · 104 citations

    3

    h-index

  4. International Journal of Refrigeration

    3 publications · 197 citations

    3

    h-index

  5. Computers & Fluids

    2 publications · 34 citations

    2

    h-index

1–5