An optical technique is described that is often used nowadays to measure su
rface pressures on wind tunnel models and flight vehicles. The technique us
es luminescent coatings, which are painted on the model surface, excited by
light of appropriate wavelength, and imaged with digital cameras. The inte
nsity of the emitted light is inversely proportional to the surface pressur
e. Hence, the surface pressures can be measured efficiently and affordably
with a high spatial resolution. The theory and chemistry of how such coatin
gs work and the parameters that affect them are presented. The required har
dware and software are described, with emphasis on the different measuremen
t systems and procedures. The various error sources are discussed, and corr
ection schemes that can be used to minimize them are presented. Sample resu
lts, covering a wide range of conditions and applications, are presented an
d discussed.