Minimum Length Nozzle is a type of converging-diverging nozzle designed to achieve supersonic flow expansion in the shortest possible axial length by employing a contoured throat region that eliminates flow separation and ensures isentropic acceleration from subsonic to supersonic velocities.
10
Publications
239
Citations
15
Authors
6
Institutions
Publications per year
2017–2026
1
Variants
Minimum Length Nozzle
Parents
Publications
10
Comparison of Minimum Length Nozzles
Brian Argrow, George Emanuel · Journal of Fluids Engineering · 1988 · 62 citations
Minimum Length Axisymmetric Laval Nozzles
LUCIAN Z. DUMIRESCU · AIAA Journal · 1975 · 27 citations
Engineering, Aerospace Engineering, Mechanical Engineering +9
1–5 of 10
Authors
15
- TZ
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- BA
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- GE
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- ZY
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- YZ
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1–5 of 15
Institutions
6
University of Blida
Blida, Algeria
4 h-index
8 publications
126 citations
University of Oklahoma
Norman, United States
2 h-index
4 publications
162 citations
University of Colorado Boulder
Boulder, United States
1 h-index
2 publications
54 citations
Instituto de Aeronáutica e Espaço
São José dos Campos, Brazil
1 h-index
2 publications
20 citations
Nagoya University
Nagoya, Japan
1 h-index
2 publications
38 citations
Zhejiang University
Hangzhou, China
1 h-index
4 publications
56 citations
Vellore Institute of Technology University
Vellore, India
1 publications
18 citations
Saveetha University
Chennai, India
1 publications
18 citations
1–8 of 6
Venues
- Journal of Fluids Engineering
3 publications · 108 citations
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- AIAA Journal
1 publications · 27 citations
1
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- Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering
1 publications · 14 citations
1
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- Advances in Space Research
1 publications · 26 citations
1
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- Chinese Journal of Aeronautics
CJA · 1 publications · 22 citations
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