Stall Boundary Analysis

Stall Boundary Analysis is a methodological framework within flight envelope characterization that identifies and quantifies the aerodynamic limits of an aircraft's operational envelope where airflow separation leads to loss of lift, distinguishing itself by systematically modeling the onset of stall conditions across varying flight parameters.

13

Publications

484

Citations

41

Authors

20

Institutions

Publications per year

2017–2026

5

Authors

41

  1. XS
    Xiaofeng Sun

    Beihang University, China

    3 publications · 52 citations

    3

    h-index

  2. MV
    Mehdi Vahdati

    Imperial College London, United Kingdom

    3 publications · 238 citations

    3

    h-index

  3. DS
    Dakun Sun

    Beihang University, China

    2 publications · 39 citations

    2

    h-index

  4. CB
    Christoph Brandstetter

    Laboratoire de Mécanique des Fluides et d'Acoustique, France

    2 publications · 37 citations

    2

    h-index

  5. SS
    Sina Stapelfeldt

    Imperial College London, United Kingdom

    2 publications · 37 citations

    2

    h-index

1–5 of 41

Venues

  1. Journal of Turbomachinery

    5 publications · 234 citations

    5

    h-index

  2. AIAA Journal

    2 publications · 91 citations

    2

    h-index

  3. 1

    h-index

  4. Journal of Propulsion and Power

    1 publications · 62 citations

    1

    h-index

  5. 1

    h-index

1–5