Rocket Engine Nozzles

Rocket Engine Nozzles is a specialized propulsion component that belongs to the class of fluid acceleration systems, distinguished by its precisely contoured geometry designed to expand and direct high-temperature, high-pressure combustion gases to generate thrust through controlled supersonic exhaust flow.

268

Publications

9.2K

Citations

634

Authors

189

Institutions

Publications per year

2017–2026

50

Authors

634

  1. FN
    Francesco Nasuti

    Sapienza University of Rome, Italy

    14 publications · 588 citations

    12

    h-index

  2. MO
    Marcello Onofri

    Sapienza University of Rome, Italy

    11 publications · 435 citations

    11

    h-index

  3. GH
    G. Hagemann

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

    10 publications · 932 citations

    10

    h-index

  4. MF
    Manuel Frey

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

    8 publications · 726 citations

    8

    h-index

  5. GC
    Guobiao Cai

    Beihang University, China

    8 publications · 219 citations

    8

    h-index

1–5 of 634

Venues

  1. Journal of Propulsion and Power

    39 publications · 2.1K citations

    21

    h-index

  2. AIAA Journal

    23 publications · 825 citations

    15

    h-index

  3. Acta Astronautica

    17 publications · 474 citations

    15

    h-index

  4. Aerospace Science and Technology

    AST · 14 publications · 468 citations

    14

    h-index

  5. NASA Technical Reports Server (NASA)

    Repository · 10 publications · 292 citations

    10

    h-index

1–5