Nozzle Thrust Coefficient
The Nozzle Thrust Coefficient is a dimensionless performance metric in propulsion engineering that quantifies the efficiency of a nozzle in converting propellant mass flow and chamber pressure into thrust, defined as the ratio of actual thrust produced to the ideal thrust under reference conditions.
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2017–2026
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Effects of the nozzle configuration on solar-powered variable geometry ejectors
Zuozhou Chen, Xu Jin, Akihiko Shimizu et al. · Solar Energy · 2017 · 50 citations
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Langley Research Center
Hampton, United States
5 h-index
10 publications
294 citations

Nanjing University of Aeronautics and Astronautics
Nanjing, China
3 h-index
16 publications
447 citations

Ames Research Center
Mountain View, United States
3 h-index
3 publications
56 citations

Glenn Research Center
Cleveland, United States
3 h-index
5 publications
191 citations
Lockheed Martin (United States)
Bethesda, United States
3 h-index
8 publications
408 citations
Virginia Tech
Blacksburg, United States
2 h-index
2 publications
44 citations

Sapienza University of Rome
Rome, Italy
2 h-index
6 publications
141 citations

Beihang University
Beijing, China
2 h-index
3 publications
42 citations
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