We describe a fibre Fabry-Perot heat-transfer sensor that is capable of per
forming the high-spatial-resolution measurements required in turbomachinery
research. The all-fibre cavity operates as a calorimeter embedded perpendi
cular to the test surface. The cavity incorporates a Bragg grating as the i
nternal reflector, producing a mechanically robust sensor suitable for aero
dynamic measurements. We present experimental results from an impinging flo
w rig, comparing the optical sensor with a thin-film resistance gauge subje
cted to a step increase in heat flux of 30 kW m(-2).