Add to ORKGThe use of resin film infusion (RFI) has been proven to reduce the cost of production of aircraft secondary sandwich structure. In this paper thermoelastic stress analysis (TSA) is used to assess the performance of full scale aircraft sandwich structure panels produced using both the conventional autoclave process and RFI. Finite element (FE) models of both panel types are developed and TSA is used to validate the models
The results from an experimental and analytical study of a composite sandwich fuselage side panel fo...
The present paper provides a description of the RFI (Resin Film Infusion) method and influence of th...
The aim of this research work is to determine the maximum load carrying capacity of sandwich panels ...
The use of resin film infusion (RFI) has been proven to reduce the cost of production of aircraft se...
Full scale tests carried out on polymer composite sandwich panels, which model the loads experienced...
This paper describes the design of a test rig, which is used to apply a representative pressure load...
In the current, environmentally-aware, climate aircraft designers are under increasing pressure topr...
A study of the application of two full field optical strain analysis techniques to aircraft standard...
The objective of this research is to reduce the cost of carbon fibre sandwich component manufacture ...
Most sandwich structures are defined using a three-layer type of construction, two thin layers and a...
Composite sandwich structures are being increasingly employed in applications which require high str...
Thermoelastic stress analysis (TSA) has been applied to large scale honeycomb core sandwich structur...
This study provides a detailed consideration of five manufacturing options that are used to produc...
This work describes a sandwich composite designed for a model aircraft under Society of Automotive E...
Sandwich composite structures are a distinct category of laminated composite materials with extensiv...
The results from an experimental and analytical study of a composite sandwich fuselage side panel fo...
The present paper provides a description of the RFI (Resin Film Infusion) method and influence of th...
The aim of this research work is to determine the maximum load carrying capacity of sandwich panels ...
The use of resin film infusion (RFI) has been proven to reduce the cost of production of aircraft se...
Full scale tests carried out on polymer composite sandwich panels, which model the loads experienced...
This paper describes the design of a test rig, which is used to apply a representative pressure load...
In the current, environmentally-aware, climate aircraft designers are under increasing pressure topr...
A study of the application of two full field optical strain analysis techniques to aircraft standard...
The objective of this research is to reduce the cost of carbon fibre sandwich component manufacture ...
Most sandwich structures are defined using a three-layer type of construction, two thin layers and a...
Composite sandwich structures are being increasingly employed in applications which require high str...
Thermoelastic stress analysis (TSA) has been applied to large scale honeycomb core sandwich structur...
This study provides a detailed consideration of five manufacturing options that are used to produc...
This work describes a sandwich composite designed for a model aircraft under Society of Automotive E...
Sandwich composite structures are a distinct category of laminated composite materials with extensiv...
The results from an experimental and analytical study of a composite sandwich fuselage side panel fo...
The present paper provides a description of the RFI (Resin Film Infusion) method and influence of th...
The aim of this research work is to determine the maximum load carrying capacity of sandwich panels ...