Rotorcraft Structural Optimization

Rotorcraft Structural Optimization is a computational and analytical framework that systematically enhances the performance, efficiency, and reliability of rotorcraft structural systems by minimizing weight and material usage while satisfying aeromechanical, dynamic, and safety constraints inherent to rotary-wing flight.

22

Publications

621

Citations

51

Authors

21

Institutions

Publications per year

2017–2026

2

Authors

51

  1. HM
    H. M. Adelman

    Langley Research Center, United States

    3 publications · 73 citations

    3

    h-index

  2. WR
    Wayne R. Mantay

    Langley Research Center, United States

    2 publications · 53 citations

    2

    h-index

  3. JL
    Joanne L. Walsh

    Langley Research Center, United States

    2 publications · 33 citations

    2

    h-index

  4. PP
    Peretz P. Friedmann

    University of Michigan, United States

    2 publications · 115 citations

    2

    h-index

  5. SS
    SangJoon Shin

    Seoul National University, South Korea

    2 publications · 25 citations

    2

    h-index

1–5 of 51

Venues

  1. Journal of Aircraft

    5 publications · 246 citations

    5

    h-index

  2. 2

    h-index

  3. AIAA Journal

    2 publications · 39 citations

    2

    h-index

  4. 1

    h-index

  5. 1

    h-index

1–5