Conventional twist drilling is a widely used machining process for creating holes in aerospace and automobile structures. Drilling at room temperature can sometime affect the quality of machined holes due to increased thermal effects on the workpiece. Thermal effects can be a cumbersome when machining composites and fibre metal laminates due to their different thermal expansion coefficients, which may introduce additional stress in the structure. Thermal machining effects can be minimised using coolants supplied either directly or indirectly to the cutting tool-workpiece interaction zone, to remove away part of the generated heat. The use of coolants adds extra costs for handling, disposal and environmental impact. Therefore, environmental...
In recent years, there has been a substantial growth in the application of carbon fiber reinforced p...
Fibre metal laminates (FMLs) are a special type of hybrid materials, which consist of sheets of meta...
Defects during the drilling process in carbon fibre laminates can result in late stage rejections in...
Conventional twist drilling is a widely used machining process for creating holes in aerospace and a...
Abstract The interest on fiber metal laminates has increased significantly in recent years as a cons...
WOS:000642066300003GLARE? is a composite-metal laminate currently used in the Airbus A380 fuselage d...
The cooling technology used in the machining process can influence the surface integrity of aerospac...
The present thesis investigates the machining performance of an aerospace structural material comme...
The current study investigates the influence of applying cryogenic liquid nitrogen cooling and minim...
S2 glass fibre reinforced epoxy composites are widely used in aeronautical applications owing to the...
The rise in cutting temperatures during the machining process can influence the final quality of the...
The rise in cutting temperatures during the machining process can influence the final quality of the...
Machining Glass fibre aluminium reinforced epoxy (GLARE) is cumbersome due to distinctively differen...
Fibre metal laminates (FMLs) are multilayered metal composite materials currently used in aeronautic...
Fibre metal laminates (FMLs) are multilayered metal composite materials currently used in aeronautic...
In recent years, there has been a substantial growth in the application of carbon fiber reinforced p...
Fibre metal laminates (FMLs) are a special type of hybrid materials, which consist of sheets of meta...
Defects during the drilling process in carbon fibre laminates can result in late stage rejections in...
Conventional twist drilling is a widely used machining process for creating holes in aerospace and a...
Abstract The interest on fiber metal laminates has increased significantly in recent years as a cons...
WOS:000642066300003GLARE? is a composite-metal laminate currently used in the Airbus A380 fuselage d...
The cooling technology used in the machining process can influence the surface integrity of aerospac...
The present thesis investigates the machining performance of an aerospace structural material comme...
The current study investigates the influence of applying cryogenic liquid nitrogen cooling and minim...
S2 glass fibre reinforced epoxy composites are widely used in aeronautical applications owing to the...
The rise in cutting temperatures during the machining process can influence the final quality of the...
The rise in cutting temperatures during the machining process can influence the final quality of the...
Machining Glass fibre aluminium reinforced epoxy (GLARE) is cumbersome due to distinctively differen...
Fibre metal laminates (FMLs) are multilayered metal composite materials currently used in aeronautic...
Fibre metal laminates (FMLs) are multilayered metal composite materials currently used in aeronautic...
In recent years, there has been a substantial growth in the application of carbon fiber reinforced p...
Fibre metal laminates (FMLs) are a special type of hybrid materials, which consist of sheets of meta...
Defects during the drilling process in carbon fibre laminates can result in late stage rejections in...