Thrust-to-weight Optimization

Thrust-To-Weight Optimization is a performance-driven engineering methodology within aerospace systems design that specifically involves the systematic adjustment and balancing of an aircraft's thrust output relative to its total weight to achieve optimal acceleration, stability, and efficiency during autonomous takeoff.

24

Publications

958

Citations

85

Authors

35

Institutions

Publications per year

2017–2026

6

Authors

85

  1. JW
    Jue Wang

    Nantong University, China

    1 publications · 10 citations

    1

    h-index

  2. ZW
    Zishen Wan

    Georgia Institute of Technology, United States

    1 publications · 33 citations

    1

    h-index

  3. JC
    Junghwan Chang

    Dong-A University, South Korea

    1 publications · 24 citations

    1

    h-index

  4. RM
    Rula M. Coroneos

    Glenn Research Center, United States

    1 publications · 10 citations

    1

    h-index

  5. WT
    Wanbin Tang

    University of Electronic Science and Technology of China, China

    1 publications · 63 citations

    1

    h-index

1–5 of 85

Venues

  1. Journal of Guidance Control and Dynamics

    5 publications · 297 citations

    5

    h-index

  2. Journal of Propulsion and Power

    2 publications · 48 citations

    2

    h-index

  3. Journal of Aircraft

    1 publications · 10 citations

    1

    h-index

  4. IEEE Transactions on Magnetics

    1 publications · 24 citations

    1

    h-index

  5. Aerospace

    1 publications · 12 citations

    1

    h-index

1–5