Description: Investigation of the aerodynamic drag of several jet noise suppressors over a range of Mach numbers and several nozzle pressure ratios. The least drag was caused by lobe-type suppressors. The eight-lobe nozzle with ejector caused the greatest amount of drag.
Date: April 1958
Creator: North, Warren J.
Item Type: Refine your search to only Report
Partner: UNT Libraries Government Documents Department