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.

48

Publications

1.1K

Citations

124

Authors

40

Institutions

Publications per year

2017–2026

15

Authors

124

  1. KY
    Kaikai Yu

    Nanjing University of Aeronautics and Astronautics, China

    3 publications · 84 citations

    3

    h-index

  2. JX
    Jinglei Xu

    Nanjing University of Aeronautics and Astronautics, China

    3 publications · 84 citations

    3

    h-index

  3. JW
    Jeffrey W. Hamstra

    Lockheed Martin (United States), United States

    2 publications · 102 citations

    2

    h-index

  4. SH
    Shuai Huang

    Nanjing University of Aeronautics and Astronautics, China

    2 publications · 57 citations

    2

    h-index

  5. DG
    Daniel G. Schauerhamer

    Langley Research Center, United States

    2 publications · 43 citations

    2

    h-index

1–5 of 124

Venues

  1. Journal of Spacecraft and Rockets

    4 publications · 95 citations

    4

    h-index

  2. NASA STI Repository (National Aeronautics and Space Administration)

    Repository · 3 publications · 123 citations

    3

    h-index

  3. Journal of Propulsion and Power

    3 publications · 44 citations

    3

    h-index

  4. AIAA Journal

    3 publications · 105 citations

    3

    h-index

  5. Physics of Fluids

    1 publications · 13 citations

    2

    h-index

1–5