Blade Tip Clearance is the radial distance between the tip of a turbofan engine blade and the surrounding casing, distinguishing it as a critical aerodynamic parameter influencing engine efficiency, performance, and blade dynamics.
583
Publications
21.9K
Citations
1.3K
Authors
334
Institutions
Publications per year
2017–2026
126
Variants
Tip Clearance
Parents
Publications
583
Criteria for Spike Initiated Rotating Stall
Huu Duc Vo, C. S. Tan, E. M. Greitzer · Journal of Turbomachinery · 2008 · 496 citations
Tip Leakage Flow in Axial Compressors
J. A. Storer, N. A. Cumpsty · Journal of Turbomachinery · 1991 · 306 citations
1–5 of 583
Authors
1.3K
- NA
11
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- HD
11
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- JH
10
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- EM
10
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- CS
9
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1–5 of 1.3K
Institutions
334
Glenn Research Center
Cleveland, United States
26 h-index
87 publications
4.1K citations
University of Cambridge
Cambridge, United Kingdom
20 h-index
51 publications
3.8K citations
Texas A&M University
College Station, United States
15 h-index
41 publications
2.9K citations
Northwestern Polytechnical University
Xi'an, China
15 h-index
74 publications
1.7K citations
General Electric (United States)
Boston, United States
13 h-index
28 publications
1.4K citations
Beihang University
Beijing, China
12 h-index
56 publications
1.4K citations
Chinese Academy of Sciences
Beijing, China
12 h-index
47 publications
1.3K citations
Massachusetts Institute of Technology
Cambridge, United States
12 h-index
21 publications
2.9K citations
1–8 of 334
Venues
- Journal of Turbomachinery
115 publications · 7.7K citations
47
h-index
- Journal of Propulsion and Power
25 publications · 818 citations
19
h-index
- Journal of Engineering for Gas Turbines and Power
19 publications · 672 citations
16
h-index
- Proceedings of the Institution of Mechanical Engineers Part A Journal of Power and Energy
21 publications · 495 citations
14
h-index
- Volume 1: Turbomachinery
Conference · 20 publications · 459 citations
13
h-index
1–5