A wind-tunnel investigation of the characteristics of the surface pres
sures on the vertical fin of a rigid 6% scale model of the F/A-18 due
to buffet has been conducted in the Institute for Aerospace Research (
IAR) 1.5-m trisonic blowdown wind tunnel. The measurements were carrie
d out by means of 48 fast response pressure transducers installed dire
ctly opposite to each other on the fin surfaces. Time-averaged and rms
pressure distributions at various angles of attack were determined to
investigate the behavior of the pressures on the fin surfaces. Space-
time correlations of the transducer signals were performed to obtain t
he broadband eddy scale and convection pattern of the pressure field.
The buffet loads were calculated from summation of the pressure signal
s on the vertical fin surfaces. Spectral analyses and probability dens
ities were evaluated to provide statistical information on the charact
eristics of the buffet loads.