Propulsion System Sizing is a systematic engineering process within propulsion system integration that determines the optimal physical and performance characteristics of a propulsion unit to meet specific mission requirements, aircraft constraints, and efficiency targets while differentiating from related design and optimization activities by its focus on initial dimensioning and capability alignment.
50
Publications
1.6K
Citations
144
Authors
44
Institutions
Publications per year
2017–2026
20
Publications
50
1–5 of 50
Authors
144
- DN
8
h-index
- MH
3
h-index
- DS
3
h-index
- IC
3
h-index
- GS
2
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1–5 of 144
Institutions
44
Georgia Institute of Technology
Atlanta, United States
7 h-index
18 publications
329 citations
RMIT University
Melbourne, Australia
2 h-index
5 publications
220 citations
Auburn University
Auburn, United States
2 h-index
4 publications
104 citations
Bauhaus Luftfahrt
Munich, Germany
2 h-index
8 publications
496 citations
Delft University of Technology
Delft, The Netherlands
2 h-index
6 publications
519 citations
Technical University of Munich
Munich, Germany
2 h-index
3 publications
69 citations
Pace University
New York, United States
2 h-index
3 publications
51 citations
Nantes Université
Nantes, France
2 h-index
6 publications
216 citations
1–8 of 44
Venues
- Journal of Aircraft
7 publications · 411 citations
7
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- CEAS Aeronautical Journal
3 publications · 61 citations
3
h-index
- Aerospace
3 publications · 114 citations
3
h-index
- Journal of Spacecraft and Rockets
2 publications · 52 citations
2
h-index
- 3rd International Energy Conversion Engineering Conference
Conference · 2 publications · 42 citations
2
h-index
1–5