Engine Weight Reduction

Engine Weight Reduction is a methodological advancement in aerospace engineering that systematically minimizes the structural mass of turbofan engines while preserving or enhancing performance, safety, and durability requirements.

72

Publications

3.1K

Citations

231

Authors

85

Institutions

Publications per year

2017–2026

13

Authors

231

  1. CN
    Craig Neuroth

    United States Air Force Research Laboratory, United States

    2 publications · 33 citations

    2

    h-index

  2. KS
    Kazuo Shibata

    Tokyo Institute of Technology, Japan

    2 publications · 87 citations

    2

    h-index

  3. BS
    Balu Sekar

    United States Air Force Research Laboratory, United States

    2 publications · 29 citations

    2

    h-index

  4. DS
    Dale Shouse

    United States Air Force Research Laboratory, United States

    2 publications · 33 citations

    2

    h-index

  5. MP
    Marco Pierini

    University of Florence, Italy

    2 publications · 69 citations

    2

    h-index

1–5 of 231

Venues

  1. 5

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  2. NASA Technical Reports Server (NASA)

    Repository · 3 publications · 99 citations

    3

    h-index

  3. MTZ worldwide

    3 publications · 33 citations

    3

    h-index

  4. Advanced Engineering Materials

    2 publications · 28 citations

    2

    h-index

  5. Materials Science and Technology

    MST · 2 publications · 109 citations

    2

    h-index

1–5