Buoyancy forces are known to alter the burning velocity of a turbulent
flame by modifying the flame wrinkling process. To quantify how dame
wrinkles are amplified or attenuated by buoyancy, a repeatable wrinkle
of known size and amplitude is created in a premixed dame by interact
ing the dame with a vortex. Images of the wrinkle amplitude were obtai
ned for microgravity conditions in the NASA Lewis Research Center 2.2-
s drop tower and for l-g conditions. Both thermodiffusively stable and
unstable cases were considered. Results quantify the degree to which
buoyancy suppresses the flame wrinkling; where buoyancy is removed, th
e microgravity flames have a wrinkle amplitude that is 2-3 times great
er than 1-g flames. Flame stretch effects also are observed because th
e diffusionally unstable flames have larger wrinkle amplitudes than th
e stable cases. The particle imaging velocimetry velocity data show th
at two stabilizing mechanisms occur due to buoyancy: the conventional
Rayleigh-Taylor mechanism and a baroclinic stabilization mechanism, wh
ich has not been observed previously in combustion processes, Measurem
ents show that the flame generates new vorticity, and this flame-gener
ated vorticity can help to suppress the flame wrinkling.