Postbuckling analyses and derivations of Knockdown factors for hybrid-grid stiffened cylinders-Reference-Cited by-同舟云学术

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Postbuckling analyses and derivations of Knockdown factors for hybrid-grid stiffened cylinders

Published:2018-11 Issue: Volume:82-83 Page:20-31
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Sim Chang-Hoon,Park Jae-Sang^ORCID,Kim Han-Il,Lee Ye-Lin,Lee Keejoo

Funder

Korea Aerospace Research Institute

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference23 articles.

1. Buckling of Thin-Walled Circular Cylinders;Weingarten,1968

2. Future directions and challenges in shell stability analysis;Arbocz;Thin-Walled Struct.,2012

3. Developing the next generation shell buckling design factors and technologies;Hilburger,2012

4. Comparison of methods to predict lower bound buckling loads of cylinders under axial compression;Haynie,2010

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1. Neural network-based DPIM for uncertainty quantification of imperfect cylindrical stiffened shells with multiple random parameters;Engineering Analysis with Boundary Elements;2024-09

2. Local damage and imperfection sensitivities of pyramidal core sandwich cylinders;Thin-Walled Structures;2024-08

3. Investigation of Buckling Knockdown Factors for Pressurized Metallic Cylinders Using Various Numerical Modeling Techniques of Initial Imperfections;International Journal of Aeronautical and Space Sciences;2023-10-08

4. Numerical vibration correlation technique analyses for composite cylinder under compression and internal pressure;STRUCT ENG MECH;2023

5. Imperfection Insensitivity of Origami-Inspired Tubular Structures;Acta Mechanica Solida Sinica;2023-06-14

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