An experimental investigation was undertaken to examine the effect of cavit
y lateral width on the flow oscillations that occur in an open cavity place
d within a turbulent subsonic boundary layer. A rectangular cavity with a l
ength to depth ratio L/D = 1 and planform aspect ration L/W = 0.115 was pla
ced within a thick turbulent boundary layer with a corresponding Re-theta =
10.5 x 10(3). Pressure time histories were acquired at six separate cavity
widths (or L/W values) using microphone-type pressure transducers. The spe
ctral character of these signals was analyzed and the pressure levels and d
ominant frequencies determined. This study indicates that large changes in
the pressure level occur as L/W varies from 0.115 to 0.682. A state of flui
d dynamic resonance was observed at L/W = 0.137 and fluid-acoustic resonanc
e at L/W = 0.682, the smallest cavity width. Relative sound pressure level
calculations indicate that the energy within the cavity compared with that
of the boundary layer, was observed to increase by approximately 40 percent
at L/W = 0.137. [S0098-2202(00)00601-5].