Aerodynamic Thrust Vectoring

Aerodynamic Thrust Vectoring is a thrust vector control method that achieves directional control of a propulsion system by altering the external aerodynamic forces and flow fields around the exhaust plume, rather than modifying internal nozzle geometry or flow injection.

102

Publications

3.2K

Citations

206

Authors

64

Institutions

Publications per year

2017–2026

14

Authors

206

  1. KD
    Karen Deere

    Langley Research Center, United States

    6 publications · 410 citations

    6

    h-index

  2. BL
    B. L. Berrier

    Langley Research Center, United States

    5 publications · 198 citations

    5

    h-index

  3. BG
    Benjamin Gal‐Or

    Technion – Israel Institute of Technology, Israel

    5 publications · 81 citations

    5

    h-index

  4. WC
    William Crowther

    University of Manchester, United Kingdom

    5 publications · 234 citations

    5

    h-index

  5. MF
    Michele Ferlauto

    Politecnico di Torino, Italy

    5 publications · 84 citations

    5

    h-index

1–5 of 206

Venues

  1. NASA Technical Reports Server (NASA)

    Repository · 5 publications · 151 citations

    5

    h-index

  2. Journal of Propulsion and Power

    5 publications · 136 citations

    5

    h-index

  3. AIAA Journal

    4 publications · 157 citations

    4

    h-index

  4. 4

    h-index

  5. Journal of Aircraft

    3 publications · 70 citations

    3

    h-index

1–5