Compressor Stall

Compressor Stall is a fluid dynamic instability within gas turbine engines characterized by the breakdown of steady axial airflow through the compressor, resulting in a localized or complete reversal of flow due to excessive pressure rise and adverse pressure gradients exceeding the blade aerodynamic limits.

640

Publications

28K

Citations

1.1K

Authors

271

Institutions

Publications per year

2017–2026

143

Authors

1.1K

  1. EM
    E. M. Greitzer

    Massachusetts Institute of Technology, United States

    42 publications · 4.9K citations

    30

    h-index

  2. IJ
    I. J. Day

    University of Cambridge, United Kingdom

    28 publications · 3.4K citations

    24

    h-index

  3. JD
    Juan Du

    Institute of Engineering Thermophysics, China

    20 publications · 612 citations

    17

    h-index

  4. DS
    Dakun Sun

    Beihang University, China

    24 publications · 720 citations

    17

    h-index

  5. JP
    James Paduano

    Massachusetts Institute of Technology, United States

    16 publications · 1.2K citations

    16

    h-index

1–5 of 1.1K

Venues

  1. Journal of Turbomachinery

    128 publications · 9.5K citations

    54

    h-index

  2. Aerospace Science and Technology

    AST · 41 publications · 1.2K citations

    23

    h-index

  3. 19

    h-index

  4. Journal of Propulsion and Power

    32 publications · 1.3K citations

    19

    h-index

  5. Volume 1: Turbomachinery

    Conference · 19 publications · 563 citations

    15

    h-index

1–5