Publication Date:
2019-07-13
Description:
Experiments were performed to check the applicability of existing acoustic liner design procedures. The performance of three different liner configurations was tested in a duct containing three-dimensional wave motion and a one-dimensional mean flow past the liner surface. Both the local liner admittance and the overall wave attenuation provided by various liner-nozzle combinations were measured with sonic flow at the nozzle throat. The experimental data are compared with predictions from current theoretical analyses, and the comparison is used to evaluate the theories.
Keywords:
FLUID MECHANICS
Type:
AIAA PAPER 74-61
,
Aerospace Sciences Meeting; Jan 30, 1974 - Feb 01, 1974; Washington, DC
Format:
text
Permalink