Transonic Flutter Analysis

Transonic Flutter Analysis is a computational and mathematical framework within aeroelasticity that specifically characterizes the onset of dynamic instability in lifting surfaces undergoing small-amplitude oscillations in the transonic flow regime, where nonlinear effects such as shock wave formation and boundary layer interaction distinguish it from flutter analysis in purely subsonic or supersonic conditions.

122

Publications

4K

Citations

279

Authors

94

Institutions

Publications per year

2017–2026

24

Authors

279

  1. JT
    John T. Batina

    Langley Research Center, United States

    7 publications · 184 citations

    7

    h-index

  2. RM
    Robert M. Bennett

    Oregon Health & Science University, United States

    6 publications · 353 citations

    6

    h-index

  3. MF
    Max F. Platzer

    Naval Postgraduate School, United States

    6 publications · 126 citations

    6

    h-index

  4. TY
    T. Y. Yang

    Purdue University West Lafayette, United States

    5 publications · 125 citations

    5

    h-index

  5. JA
    John A. Ekaterinaris

    Foundation for Research and Technology Hellas, Greece

    5 publications · 100 citations

    5

    h-index

1–5 of 279

Venues

  1. Journal of Aircraft

    24 publications · 909 citations

    18

    h-index

  2. AIAA Journal

    15 publications · 1K citations

    13

    h-index

  3. Aerospace Science and Technology

    AST · 8 publications · 216 citations

    8

    h-index

  4. NASA Technical Reports Server (NASA)

    Repository · 3 publications · 137 citations

    3

    h-index

  5. Chinese Journal of Aeronautics

    CJA · 3 publications · 84 citations

    3

    h-index

1–5