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

Authors

153

  1. RS
    Ralf Stark

    Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR), Germany

    11 publications · 344 citations

    10

    h-index

  2. FN
    Francesco Nasuti

    Sapienza University of Rome, Italy

    7 publications · 215 citations

    7

    h-index

  3. MO
    Marcello Onofri

    Sapienza University of Rome, Italy

    7 publications · 215 citations

    7

    h-index

  4. EM
    Emanuele Martelli

    Sapienza University of Rome, Italy

    6 publications · 204 citations

    6

    h-index

  5. CG
    Chloé Génin

    Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR), Germany

    6 publications · 165 citations

    6

    h-index

1–5 of 153

Venues

  1. Journal of Propulsion and Power

    18 publications · 1K citations

    16

    h-index

  2. AIAA Journal

    5 publications · 160 citations

    5

    h-index

  3. Aerospace Science and Technology

    AST · 4 publications · 126 citations

    4

    h-index

  4. NASA Technical Reports Server (NASA)

    Repository · 2 publications · 109 citations

    2

    h-index

  5. 33rd Joint Propulsion Conference and Exhibit

    Conference · 2 publications · 52 citations

    2

    h-index

1–5