This study examines the energy absorption capabilities of cellular honeycombs subjected to in-plane compression. ABAQUS finite element analysis is used and cellular honeycombs with different cell geometries are considered. For various cell angles, comparison of simulation results for full size honeycombs and their single cell analogs suggest that the energy absorption can be accurately determined using the single cell model. Cell wall length study shows that the specific energy absorption (energy absorption per unit mass) is higher for cells with shorter vertical walls. Cell wall thickness study shows that increasing wall thickness increases the specific energy absorption. Vertical wall thickness study shows that the vertical walls be thick...
International audienceThis paper presents an experimental study of the compressive response of hexag...
The effective static mechanical properties, such as the moduli of elasticity and rigidity and Poisso...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76537/1/AIAA-2004-1640-728.pd
The in-plane crushing and energy absorption of sandwiched honeycomb cores with facesheets are examin...
iii In aerospace field, use of honeycombs in energy absorbing applications is a very attractive conc...
Introducing gradient into cellular materials has been envisioned as an effective way to improve thei...
Honeycomb structure is used as the shock absorbent to protect precision machines during transport. T...
From a design perspective, there are four decisions that need to be made when integrating cellular ...
The large scale and long calculation times are unavoidable problems in modeling honeycomb structures...
The y-directional mechanical properties of hexagonal honeycombs with various cell-wall angles are ex...
Nowadays, aluminium honeycomb has become well-known as a good energy absorbing cellular structure. D...
Thesis (M.S)--Wichita State University, College of Engineering, Dept. of Aerospace Engineering"Decem...
The work describes the out-of-plane properties of a curved wall honeycomb structure evaluated using ...
Honeycomb structures have applications in many engineering industries due to their desirable attribu...
The effect of cell size on the out of plane compressive crushing response of circular cell polycarbo...
International audienceThis paper presents an experimental study of the compressive response of hexag...
The effective static mechanical properties, such as the moduli of elasticity and rigidity and Poisso...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76537/1/AIAA-2004-1640-728.pd
The in-plane crushing and energy absorption of sandwiched honeycomb cores with facesheets are examin...
iii In aerospace field, use of honeycombs in energy absorbing applications is a very attractive conc...
Introducing gradient into cellular materials has been envisioned as an effective way to improve thei...
Honeycomb structure is used as the shock absorbent to protect precision machines during transport. T...
From a design perspective, there are four decisions that need to be made when integrating cellular ...
The large scale and long calculation times are unavoidable problems in modeling honeycomb structures...
The y-directional mechanical properties of hexagonal honeycombs with various cell-wall angles are ex...
Nowadays, aluminium honeycomb has become well-known as a good energy absorbing cellular structure. D...
Thesis (M.S)--Wichita State University, College of Engineering, Dept. of Aerospace Engineering"Decem...
The work describes the out-of-plane properties of a curved wall honeycomb structure evaluated using ...
Honeycomb structures have applications in many engineering industries due to their desirable attribu...
The effect of cell size on the out of plane compressive crushing response of circular cell polycarbo...
International audienceThis paper presents an experimental study of the compressive response of hexag...
The effective static mechanical properties, such as the moduli of elasticity and rigidity and Poisso...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76537/1/AIAA-2004-1640-728.pd