Bell Nozzles
Bell Nozzle is a type of convergent-divergent rocket nozzle characterized by its contoured, bell-shaped profile that optimizes thrust by efficiently expanding exhaust gases to supersonic velocities within a compact axial length.
65
Publications
2.1K
Citations
153
Authors
53
Institutions
Publications per year
2017–2026
12
Variants
Bell Nozzle
Parents
65
G. Hagemann, H. Immich, Thong Van Nguyen et al. · Journal of Propulsion and Power · 1998 · 281 citations
Engineering, Aerospace Engineering, Mechanical Engineering +16
Dual-bell altitude compensating nozzles
Martin Horn, S. S. Fisher · NASA Technical Reports Server (NASA) · 1993 · 96 citations · Full text
Critical Assessment of Dual-Bell Nozzles
Manuel Frey, G. Hagemann · Journal of Propulsion and Power · 1999 · 70 citations
1–5 of 65
153
Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR), Germany
11 publications · 344 citations
10
h-index
7
h-index
7
h-index
6
h-index
Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR), Germany
6 publications · 165 citations
6
h-index
1–5 of 153
53
Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR)
Cologne, Germany
11 h-index
31 publications
1.2K citations

Sapienza University of Rome
Rome, Italy
7 h-index
19 publications
623 citations
National Aerospace Laboratories
Bengaluru, India
4 h-index
7 publications
183 citations
Mitsubishi Heavy Industries (Japan)
Tokyo, Japan
3 h-index
5 publications
104 citations

Université d'Évry Val-d'Essonne
Évry-Courcouronnes, France
2 h-index
3 publications
79 citations
The University of Osaka
Osaka, Japan
2 h-index
9 publications
142 citations
RWTH Aachen University
Aachen, Germany
2 h-index
4 publications
45 citations
Government Medical College
Thrissur, India
2 h-index
3 publications
44 citations
1–8 of 53
18 publications · 1K citations
16
h-index
5 publications · 160 citations
5
h-index
AST · 4 publications · 126 citations
4
h-index
Repository · 2 publications · 109 citations
2
h-index
Conference · 2 publications · 52 citations
2
h-index
1–5