Annular Combustors
Annular Combustor is a continuous, ring-shaped combustion chamber in gas turbine engines that, unlike can or cannular configurations, provides a compact and aerodynamically efficient design by enclosing the turbine shaft axis in a single annular chamber where fuel and air are mixed and combusted circumferentially.
383
Publications
14.2K
Citations
843
Authors
219
Institutions
Publications per year
2017–2026
127
Variants
Annular Combustor
Parents
383
1–5 of 383
843
16
h-index
16
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Norwegian University of Science and Technology, Norway
13 publications · 792 citations
12
h-index
11
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11
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1–5 of 843
219

Centre National de la Recherche Scientifique
Paris, France
24 h-index
107 publications
5.5K citations
University of Cambridge
Cambridge, United Kingdom
21 h-index
50 publications
2.8K citations
Norwegian University of Science and Technology
Trondheim, Norway
17 h-index
35 publications
1.2K citations
Technische Universität Berlin
Berlin, Germany
16 h-index
37 publications
1.3K citations
Safran (France)
Paris, France
14 h-index
16 publications
1K citations
CentraleSupélec
Gif-sur-Yvette, France
13 h-index
57 publications
2.1K citations
Université Paris-Saclay
Gif-sur-Yvette, France
13 h-index
58 publications
2.1K citations
Laboratoire d'Énergétique Moléculaire et Macroscopique, Combustion
Gif-sur-Yvette, France
12 h-index
54 publications
3.1K citations
1–8 of 219
58 publications · 2.3K citations
27
h-index
20 publications · 1.4K citations
19
h-index
18 publications · 624 citations
16
h-index
15 publications · 1.1K citations
15
h-index
9 publications · 262 citations
10
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1–5