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
A finite element (FE) model is developed to study the structural performance on a composite wing of ...
Composite sandwich structures are being increasingly employed in applications which require high str...
Vacuum assisted resin infusion process (VARI) is a high performance and cost effective manufacturing...
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...
The objective of this research is to reduce the cost of carbon fibre sandwich component manufacture ...
Thermoelastic stress analysis (TSA) has been applied to large scale honeycomb core sandwich structur...
A study of the application of two full field optical strain analysis techniques to aircraft standard...
The paper describes the development of the application of thermoelastic stress analysis (TSA) to com...
This study provides a detailed consideration of five manufacturing options that are used to produce ...
In the current, environmentally-aware, climate aircraft designers are under increasing pressure topr...
This study provides a detailed consideration of five manufacturing options that are used to produc...
A finite element (FE) model is developed to study the structural performance on a composite wing of ...
An emerging technology need for capturing 3-D panel thermoelastic response with 2-D planar finite el...
A finite element (FE) model is developed to study the structural performance on a composite wing of ...
Composite sandwich structures are being increasingly employed in applications which require high str...
Vacuum assisted resin infusion process (VARI) is a high performance and cost effective manufacturing...
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...
The objective of this research is to reduce the cost of carbon fibre sandwich component manufacture ...
Thermoelastic stress analysis (TSA) has been applied to large scale honeycomb core sandwich structur...
A study of the application of two full field optical strain analysis techniques to aircraft standard...
The paper describes the development of the application of thermoelastic stress analysis (TSA) to com...
This study provides a detailed consideration of five manufacturing options that are used to produce ...
In the current, environmentally-aware, climate aircraft designers are under increasing pressure topr...
This study provides a detailed consideration of five manufacturing options that are used to produc...
A finite element (FE) model is developed to study the structural performance on a composite wing of ...
An emerging technology need for capturing 3-D panel thermoelastic response with 2-D planar finite el...
A finite element (FE) model is developed to study the structural performance on a composite wing of ...
Composite sandwich structures are being increasingly employed in applications which require high str...
Vacuum assisted resin infusion process (VARI) is a high performance and cost effective manufacturing...