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
Variants
Compressor Stalling
640
Criteria for Spike Initiated Rotating Stall
Huu Duc Vo, C. S. Tan, E. M. Greitzer · Journal of Turbomachinery · 2008 · 496 citations
Stall Inception in Axial Flow Compressors
I. J. Day · Journal of Turbomachinery · 1993 · 492 citations
Stall, Surge, and 75 Years of Research
I. J. Day · Journal of Turbomachinery · 2015 · 429 citations
1–5 of 640
1.1K
30
h-index
24
h-index
17
h-index
17
h-index
16
h-index
1–5 of 1.1K
271
Massachusetts Institute of Technology
Cambridge, United States
37 h-index
140 publications
12.7K citations
University of Cambridge
Cambridge, United Kingdom
30 h-index
78 publications
6.7K citations

Glenn Research Center
Cleveland, United States
25 h-index
61 publications
4.2K citations

Beihang University
Beijing, China
24 h-index
167 publications
4.5K citations

Northwestern Polytechnical University
Xi'an, China
20 h-index
140 publications
3.2K citations
Institute of Engineering Thermophysics
Beijing, China
19 h-index
104 publications
3.2K citations

Chinese Academy of Sciences
Beijing, China
19 h-index
111 publications
3.1K citations
Hartford Financial Services (United States)
Hartford, United States
16 h-index
25 publications
1.4K citations
1–8 of 271
128 publications · 9.5K citations
54
h-index
AST · 41 publications · 1.2K citations
23
h-index
22 publications · 994 citations
19
h-index
32 publications · 1.3K citations
19
h-index
Conference · 19 publications · 563 citations
15
h-index
1–5