Access the full text.
Sign up today, get DeepDyve free for 14 days.
H.R. Joshi (2013)
FE analysis of effective mechanical properties
D. Song, Xiazi Xiao, J. Xue, H. Chu, H. Duan (2015)
Mechanical properties of irradiated multi-phase polycrystalline BCC materialsActa Mechanica Sinica, 31
L. Mizzi, D. Attard, R. Gatt, A. Poźniak, K. Wojciechowski, Joseph Grima (2015)
Influence of translational disorder on the mechanical properties of hexachiral honeycomb systemsComposites Part B-engineering, 80
A. Spadoni, M. Ruzzene (2007)
Numerical and experimental analysis of the static compliance of chiral truss-core airfoilsJournal of Mechanics of Materials and Structures, 2
A. Spadoni, M. Ruzzene (2006)
Structural and Acoustic Behavior of Chiral Truss-Core BeamsJournal of Vibration and Acoustics, 128
(2013)
FE analysis of effective mechanical properties, vibration and acoustic performance of auxetic chiral core sandwich structures
(2006)
Modeling and testing of shape memory alloy chiral honeycomb structure
A. Spadoni, M. Ruzzene, S. Gonella, F. Scarpa (2009)
Phononic properties of hexagonal chiral latticesWave Motion, 46
Yijin Chen, F. Scarpa, Yuheng Liu, J. Leng (2013)
Elasticity of anti-tetrachiral anisotropic latticesInternational Journal of Solids and Structures, 50
F. Scarpa (2006)
Modeling and testing of shape memory alloy chiral honeycomb structure. In: Proceeding of SPIE 6170Proceeding of SPIE 6170
(2015)
Equivalent elastic modulus of the honeycomb core based on FEM model
A. Alderson, K. Alderson, G. Chirima, N. Ravirala, K. Zied (2010)
The in-plane linear elastic constants and out-of-plane bending of 3-coordinated ligament and cylinder-ligament honeycombsComposites Science and Technology, 70
A. Lorato, P. Innocenti, F. Scarpa, A. Alderson, K. Alderson, K. Zied, N. Ravirala, W. Miller, Christopher Smith, K. Evans (2010)
The transverse elastic properties of chiral honeycombsComposites Science and Technology, 70
A. Bacigalupo, L. Gambarotta (2014)
Homogenization of periodic hexa- and tetrachiral cellular solidsComposite Structures, 116
W. Miller, Christopher Smith, F. Scarpa, K. Evans (2010)
Flatwise buckling optimization of hexachiral and tetrachiral honeycombsComposites Science and Technology, 70
X Zheng G Cheng (2004)
Equivalent-panel mechanics analysis of honeycomb sandwich structureJ. Proj. Rockets Missiles Guidance, 24
W Wang L Fu (2008)
The equivalent calculation and experimental study of honeycomb sandwich plates for satelliteSci. Technol. Eng., 8
Jia Jin-qing (2004)
Equivalent-panel Mechanics Analysis of Honeycomb Sandwich StructureJournal of Projectiles.Rockets.Missiles and Guidance
F. Scarpa, S. Blain, T. Lew, D. Perrott, M. Ruzzene, J. Yates (2007)
Elastic buckling of hexagonal chiral cell honeycombsComposites Part A-applied Science and Manufacturing, 38
X Liu G Fu (2001)
An equivalent single-layer model of honeycomb sandwich panelEng. Mech., A01
M Ruzzene A Spadoni (2006)
Dynamic response of chiral truss-core assembliesJ. Intell. Mater. Syst. Struct., 17
X. Zhao (2013)
Analysis of mechanical properties of deformable honeycomb structure. [Ph.D. Thesis]
N. Gaspar, X. Ren, Christopher Smith, Joseph Grima, K. Evans (2005)
Novel honeycombs with auxetic behaviourActa Materialia, 53
A. Spadoni, M. Ruzzene, F. Scarpa
Structures Journal of Intelligent Material Systems and Journal of Intelligent Material Systems and Structures Dynamic Response of Chiral Truss-core Assemblies Journal of Intelligent Material Systems and Structures Additional Services and Information for Dynamic Response of Chiral Truss-core Assembli
(2013)
Analysis of mechanical properties of deformable honeycomb structure
G. Cicala, G. Recca, L. Oliveri, Y. Perikleous, F. Scarpa, C. Lira, A. Lorato, D. Grube, G. Ziegmann (2012)
Hexachiral truss-core with twisted hemp yarns: Out-of-plane shear propertiesComposite Structures, 94
A. Alderson, K. Alderson, D. Attard, K. Evans, R. Gatt, Joseph Grima, W. Miller, N. Ravirala, Christopher Smith, K. Zied (2010)
Elastic constants of 3-, 4- and 6-connected chiral and anti-chiral honeycombs subject to uniaxial in-plane loadingComposites Science and Technology, 70
Abstract Chiral honeycomb structures have been developed in recent years, showing excellent mechanical properties, including in-plane deformation and out-of-plane bearing and vibration isolation. In this study, the 65Mn chiral structure with three ligaments was modeled and analyzed using the finite element (FE) method. The effects of the dimensionless ligament length and dimensionless ligament thickness on the in-plane equivalent elastic modulus, equivalent Poisson’s ratio, and out-of-plane shear modulus were studied. The numerical results indicate that increase of the dimensionless ligament length leads to decrease of the equivalent elastic modulus and increase of the equivalent Poisson’s ratio, whereas the out-of-plane equivalent shear modulus decreases. The results also indicate that increase of the dimensionless ligament thickness leads to increase of the equivalent elastic modulus, whereas the equivalent Poisson’s ratio remains nearly unchanged and the out-of-plane equivalent shear modulus shows a linear increase. The numerical results are verified by comparison with published experimental data. These results will provide a reference for the application of chiral structures with three ligaments in the aerospace field.
"Acta Mechanica Sinica" – Springer Journals
Published: Feb 1, 2019
Read and print from thousands of top scholarly journals.
Already have an account? Log in
Bookmark this article. You can see your Bookmarks on your DeepDyve Library.
To save an article, log in first, or sign up for a DeepDyve account if you don’t already have one.
Copy and paste the desired citation format or use the link below to download a file formatted for EndNote
Access the full text.
Sign up today, get DeepDyve free for 14 days.
All DeepDyve websites use cookies to improve your online experience. They were placed on your computer when you launched this website. You can change your cookie settings through your browser.