Nozzle Contour Optimization

Nozzle Contour Optimization is a computational and engineering method that refines the geometric shape of a nozzle’s internal surface to maximize flow efficiency and thrust performance by minimizing losses due to shock waves, flow separation, and boundary layer effects under specified operating conditions.

36

Publications

1.3K

Citations

92

Authors

42

Institutions

Publications per year

2017–2026

4

Authors

92

  1. JD
    Joe D. Hoffman

    Purdue University West Lafayette, United States

    4 publications · 68 citations

    4

    h-index

  2. HD
    H. Doyle Thompson

    Purdue University West Lafayette, United States

    2 publications · 47 citations

    2

    h-index

  3. HH
    Haukur Hafsteinsson

    Chalmers University of Technology, Sweden

    2 publications · 29 citations

    2

    h-index

  4. LE
    Lars-Erik Eriksson

    Chalmers University of Technology, Sweden

    2 publications · 29 citations

    2

    h-index

  5. DR
    Daniel R. Cuppoletti

    University of Cincinnati, United States

    2 publications · 29 citations

    2

    h-index

1–5 of 92

Venues

  1. AIAA Journal

    7 publications · 157 citations

    7

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  2. Aerospace Science and Technology

    AST · 3 publications · 74 citations

    3

    h-index

  3. Journal of Propulsion and Power

    2 publications · 49 citations

    2

    h-index

  4. 37th Joint Propulsion Conference and Exhibit

    Conference · 2 publications · 33 citations

    2

    h-index

  5. 1

    h-index

1–5