Skin-stringer Buckling

Skin-Stringer Buckling is a structural instability phenomenon in aerospace engineering wherein the interconnected skin and stringer components of an aircraft panel buckle collaboratively under compressive loading, distinguished from isolated buckling modes by the coupled behavior and load transfer between the thin skin and its stiffening stringers.

29

Publications

784

Citations

78

Authors

29

Institutions

Publications per year

2017–2026

9

Authors

78

  1. CB
    Chiara Bisagni

    Politecnico di Milano, Italy

    4 publications · 78 citations

    4

    h-index

  2. AR
    A. Raimondo

    University of Campania "Luigi Vanvitelli", Italy

    3 publications · 109 citations

    3

    h-index

  3. AR
    Aniello Riccio

    University of Campania "Luigi Vanvitelli", Italy

    3 publications · 109 citations

    3

    h-index

  4. EG
    E.S. Greenhalgh

    Imperial College London, United Kingdom

    2 publications · 67 citations

    2

    h-index

  5. FS
    F. Scaramuzzino

    University of Campania "Luigi Vanvitelli", Italy

    2 publications · 75 citations

    2

    h-index

1–5 of 78

Venues

  1. Journal of Sound and Vibration

    JSV · 4 publications · 161 citations

    4

    h-index

  2. Composite Structures

    4 publications · 132 citations

    4

    h-index

  3. Composites Part B Engineering

    3 publications · 111 citations

    3

    h-index

  4. Aircraft Engineering and Aerospace Technology

    2 publications · 34 citations

    2

    h-index

  5. International Journal of Impact Engineering

    1 publications · 49 citations

    1

    h-index

1–5