Standard

Scaling methodology for buckling of sandwich composite cylindrical structures. / Balbin, Ines Uriol; Bisagni, Chiara; Schultz, Marc R.; Hilburger, Mark W.

AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials. 210049. ed. American Institute of Aeronautics and Astronautics Inc. (AIAA), 2018. AIAA 2018-1988.

Research output: Chapter in Book/Conference proceedings/Edited volumeConference contributionScientificpeer-review

Harvard

Balbin, IU, Bisagni, C, Schultz, MR & Hilburger, MW 2018, Scaling methodology for buckling of sandwich composite cylindrical structures. in AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials. 210049 edn, AIAA 2018-1988, American Institute of Aeronautics and Astronautics Inc. (AIAA), AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2018, Kissimmee, United States, 8/01/18. https://doi.org/10.2514/6.2018-1988

APA

Balbin, I. U., Bisagni, C., Schultz, M. R., & Hilburger, M. W. (2018). Scaling methodology for buckling of sandwich composite cylindrical structures. In AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials (210049 ed.). [AIAA 2018-1988] American Institute of Aeronautics and Astronautics Inc. (AIAA). https://doi.org/10.2514/6.2018-1988

Vancouver

Balbin IU, Bisagni C, Schultz MR, Hilburger MW. Scaling methodology for buckling of sandwich composite cylindrical structures. In AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials. 210049 ed. American Institute of Aeronautics and Astronautics Inc. (AIAA). 2018. AIAA 2018-1988 https://doi.org/10.2514/6.2018-1988

Author

Balbin, Ines Uriol ; Bisagni, Chiara ; Schultz, Marc R. ; Hilburger, Mark W. / Scaling methodology for buckling of sandwich composite cylindrical structures. AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials. 210049. ed. American Institute of Aeronautics and Astronautics Inc. (AIAA), 2018.

BibTeX

@inproceedings{2ba694bf28b444bcb343701dcba6a0be,
title = "Scaling methodology for buckling of sandwich composite cylindrical structures",
abstract = "The study of the buckling behavior of large shell structures through full-size tests can be complex and expensive. Therefore, scaled structures are often preferred to investigate the buckling behavior efficiently. However, it can be difficult to design scaled structures that are representative of the full-scale structures. Herein, an analytical scaling methodology for compression-loaded sandwich composite cylinders based on the nondimensionalization of the buckling equations is presented. The methodology is used to develop scaled configurations that show a similar buckling response. Both the baseline and the scaled configurations are verified by finite-element analysis. Limitations of the methodology are discussed and are a result of neglecting the flexural anisotropy and the transverse shear compliance.",
author = "Balbin, {Ines Uriol} and Chiara Bisagni and Schultz, {Marc R.} and Hilburger, {Mark W.}",
year = "2018",
doi = "10.2514/6.2018-1988",
language = "English",
booktitle = "AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials",
publisher = "American Institute of Aeronautics and Astronautics Inc. (AIAA)",
address = "United States",
edition = "210049",
note = "AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2018 ; Conference date: 08-01-2018 Through 12-01-2018",

}

RIS

TY - GEN

T1 - Scaling methodology for buckling of sandwich composite cylindrical structures

AU - Balbin, Ines Uriol

AU - Bisagni, Chiara

AU - Schultz, Marc R.

AU - Hilburger, Mark W.

PY - 2018

Y1 - 2018

N2 - The study of the buckling behavior of large shell structures through full-size tests can be complex and expensive. Therefore, scaled structures are often preferred to investigate the buckling behavior efficiently. However, it can be difficult to design scaled structures that are representative of the full-scale structures. Herein, an analytical scaling methodology for compression-loaded sandwich composite cylinders based on the nondimensionalization of the buckling equations is presented. The methodology is used to develop scaled configurations that show a similar buckling response. Both the baseline and the scaled configurations are verified by finite-element analysis. Limitations of the methodology are discussed and are a result of neglecting the flexural anisotropy and the transverse shear compliance.

AB - The study of the buckling behavior of large shell structures through full-size tests can be complex and expensive. Therefore, scaled structures are often preferred to investigate the buckling behavior efficiently. However, it can be difficult to design scaled structures that are representative of the full-scale structures. Herein, an analytical scaling methodology for compression-loaded sandwich composite cylinders based on the nondimensionalization of the buckling equations is presented. The methodology is used to develop scaled configurations that show a similar buckling response. Both the baseline and the scaled configurations are verified by finite-element analysis. Limitations of the methodology are discussed and are a result of neglecting the flexural anisotropy and the transverse shear compliance.

UR - http://www.scopus.com/inward/record.url?scp=85044615769&partnerID=8YFLogxK

U2 - 10.2514/6.2018-1988

DO - 10.2514/6.2018-1988

M3 - Conference contribution

AN - SCOPUS:85044615769

BT - AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials

PB - American Institute of Aeronautics and Astronautics Inc. (AIAA)

T2 - AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2018

Y2 - 8 January 2018 through 12 January 2018

ER -

ID: 43799432