Takeoff Weight Limits

Takeoff Weight Limits is a performance constraint metric in aerospace engineering that specifies the maximum allowable mass at which an aircraft can safely achieve the required takeoff performance under defined operational and environmental conditions.

22

Publications

504

Citations

71

Authors

27

Institutions

Publications per year

2017–2026

8

Authors

71

  1. CC
    Cristina Cuerno

    Universidad Politécnica de Madrid, Spain

    2 publications · 40 citations

    2

    h-index

  2. RT
    Robert Tipton

    Lawrence Livermore National Laboratory, United States

    1 publications · 16 citations

    1

    h-index

  3. WB
    Włodzimierz Balicki

    Łukasiewicz Research Network - Institute of Aviation, Poland

    1 publications · 17 citations

    1

    h-index

  4. JB
    Jason Bowman

    United States Air Force Research Laboratory, United States

    1 publications · 23 citations

    1

    h-index

  5. RM
    Ruxandra Mihaela Botez

    École de Technologie Supérieure, Canada

    1 publications · 38 citations

    1

    h-index

1–5 of 71

Venues

  1. Journal of Aircraft

    6 publications · 141 citations

    6

    h-index

  2. 1

    h-index

  3. DOAJ (DOAJ: Directory of Open Access Journals)

    Repository · 1 publications · 30 citations

    1

    h-index

  4. Acta Mechanica et Automatica

    1 publications · 17 citations

    1

    h-index

  5. Aircraft Engineering and Aerospace Technology

    1 publications · 11 citations

    1

    h-index

1–5