2008-01-0391 Experimental Characterisation of Heat Transfer in Exhaust Pipe Sections
Experimental Characterisation of Heat Transfer in Exhaust Pipe Sections
Flow visualisation experiments for turbine film cooling
Flow over an aerofoil without and with a leading-edge slat at a transitional Reynolds number
Aerospace applications of luminescent paint - Part two - Heat transfer measurement
Aerospace applications of luminescent paint - Part one - Pressure measurement
Energy requirements for the flight of micro air vehicles
Free Vortex Theory for Efficiency Calculations From Annular Cascade Data (95-GT-186)
A Converging Slot-Hole Film-Cooling Geometry-Part 1: Low-Speed Flat-Plate Heat Transfer and Loss