Add to ORKGThis research paper deals with an investigation of the influence of honeycomb core compression on the mechanical properties of sandwich structures. These structures consist of prepreg facing layers and two different material types of honeycomb and are produced by modified compression molding called Crush-Core technology. Produced structures are mechanically tested in three-point bending test and subjected to low-velocity impact and Charpy impact test
Mechanical behaviour of sandwich panels under different conditions have been exp...
AbstractThe concept of combining metallic honeycomb with folded thin metallic sheets (corrugation) t...
Sandwich structural elements consist of two metallic or non-metallic laminated skins separated by a ...
In the aeronautical field, sandwich structures are widely used for secondary structures like flaps o...
In the aeronautical field, sandwich structures are widely used for secondary structures like flaps o...
International audienceIn this chapter, an original method for modeling the behavior of sandwich stru...
Abstract: A study on the effect of cell size material on the mechanical properties of honeycomb core...
ABSTRACT: This article presents results from an experimental study, investigating the effects of cor...
Nomex honeycomb is used as the predominate core material in aerospace standard sandwich structure. T...
The paper proposes first to study the behavior of honeycomb alone under uniform cyclic compression-r...
This thesis demonstrates how a certain type of a sandwich core - honeycomb is manufactured and post-...
The concept of combining metallic honeycomb with folded thin metallic sheets (corrugation) to constr...
In this chapter, an original method for modeling the behavior of sandwich structures during and aft...
Thesis (Master)--Izmir Institute of Technology, Mechanical Engineering, Izmir, 2008Includes bibliogr...
Mechanical behaviour of sandwich panels under different conditions have been exprimentally studied ...
Mechanical behaviour of sandwich panels under different conditions have been exp...
AbstractThe concept of combining metallic honeycomb with folded thin metallic sheets (corrugation) t...
Sandwich structural elements consist of two metallic or non-metallic laminated skins separated by a ...
In the aeronautical field, sandwich structures are widely used for secondary structures like flaps o...
In the aeronautical field, sandwich structures are widely used for secondary structures like flaps o...
International audienceIn this chapter, an original method for modeling the behavior of sandwich stru...
Abstract: A study on the effect of cell size material on the mechanical properties of honeycomb core...
ABSTRACT: This article presents results from an experimental study, investigating the effects of cor...
Nomex honeycomb is used as the predominate core material in aerospace standard sandwich structure. T...
The paper proposes first to study the behavior of honeycomb alone under uniform cyclic compression-r...
This thesis demonstrates how a certain type of a sandwich core - honeycomb is manufactured and post-...
The concept of combining metallic honeycomb with folded thin metallic sheets (corrugation) to constr...
In this chapter, an original method for modeling the behavior of sandwich structures during and aft...
Thesis (Master)--Izmir Institute of Technology, Mechanical Engineering, Izmir, 2008Includes bibliogr...
Mechanical behaviour of sandwich panels under different conditions have been exprimentally studied ...
Mechanical behaviour of sandwich panels under different conditions have been exp...
AbstractThe concept of combining metallic honeycomb with folded thin metallic sheets (corrugation) t...
Sandwich structural elements consist of two metallic or non-metallic laminated skins separated by a ...