Reliable measurements of unsteady pressure on the surface of thin aerodynam
ic bodies in low subsonic, unsteady flows were made using small piezoelectr
ic transducers. The hand-made transducers, calibrated against a B&K microph
one for use in experiments, were used in two sets of low speed experiments.
The first set involved a stationary aerofoil encountering a rotating, peri
odic gust as would be present in a rotor-stator interaction. The second set
involved an instrumented propeller operating behind a stationary cyclic di
stortion as would be present behind stators or guide vanes. In both sets of
experiments, reliable measurements of the small unsteady pressures on the
body surfaces were made despite difficult experimental environments.