1. Experimental and numerical investigation of Helmholtz resonators and perforated liners as attenuation devices in industrial gas turbine combustors. (1st July 2015) Authors: Houston, B.; Wang, J.; Qin, Q.; Rubini, P. Journal: Fuel Issue: Volume 151(2015) Page Start: 31 Record Type: Journal Article View Content: Available online (eLD content is only available in our Reading Rooms) ↗